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VIEWS: 55 PAGES: 12

									                          SAE AERO-DESIGN REPORT GRADESHEET
                     Team 6 - University of Cincinnati (judge wh)
                                                                                           CLASS
                                                                             Total      Regular Class
                                   47.3                                       Points
                                                                                        Open Class
                                                                            Available
                                                                                        Micro Class

Design Report                                                                  400      Awarded Pts
 FORMAT & LAYOUT                                                               60           58
   Cover Page
     School Name
     Team Name                                                                 13             13
     Team Number
     Report Title
  Statement of Compliance (Page 2 of Report)
                                                                                5             5

  Table of Contents
                                                                                5             3
     Correct and accurate page references
  Format Requirements
     Paper Size
     Font (minimum size is 12 pts proportional or a 10 character per inch
     nonproportional font)                                                     12             12
     Margins
     Binding (No loose pages)
  Page Limit Requirement
     The report must not exceed (30) thirty double-space, typewritten          10             10
     pages including appendices.
  Three (3) copies of identical Design Report
                                                                               15             15

 DESIGN PROCESS                                                                160           160
  Introduction
     Definition of the Objective                                               30             30
     Requirement Statement
  Research
     Discussion of Concepts
                                                                               40             40
     Discussion of previous design/concepts/publications
     Test & Experiment (Method and Procedures)
  Design Analysis & Review Process
                                                                               45             45
     Discussion of Results
  Design Selection Process
                                                                               45             45
     Why certain design was selected over others

 CALCULATIONS                                                                  60             60
  Performance
                                                                               12             12
     Equations, Calculation, Charts, and/or Tables
  Stability & Control
                                                                               12             12
     Equations, Calculation, Charts, and/or Tables
  Aircraft Sizing
                                                                               12             12
     Equations, Calculation, Charts, and/or Tables
  Weight Build-up and Analysis
                                                                               12             12
     Equations, Calculation, Charts, and/or Tables
  Structural Analysis
     Equations, Calculation, Charts, and/or Tables
                                                                               12             12




                                                     Page 1 of 12
                     SAE AERO-DESIGN REPORT GRADESHEET
                Team 6 - University of Cincinnati (judge wh)
                                                                    CLASS
                                                      Total      Regular Class
                      47.3                             Points
                                                                 Open Class
                                                     Available
                                                                 Micro Class

INNOVATIONS                                             50             50
 Process/methods
                                                        10             10

 Design
                                                        10             10

 Application
                                                        10             10

 Construction
                                                        10             10

 Use of Computer Aided Design tools
                                                        10             10

WRITING                                                 70             63
 Spelling
                                                        10             9

 Grammar
                                                        10             9

 Sentence structure
                                                        10             9

 Punctuation
                                                        10             9

 Clarity
                                                        10             9

 Organization
                                                        10             9

 Accurate Table and Figure identifications
                                                        10             9




                                      Page 2 of 12
                         SAE AERO-DESIGN REPORT GRADESHEET
                    Team 6 - University of Cincinnati (judge wh)
                                                                                             CLASS
                                                                               Total      Regular Class
                                47.3                                            Points
                                                                                          Open Class
                                                                              Available
                                                                                          Micro Class

Plans                                                                            50             42
   Paper Size
     Plan sheet must be ANSI B sized paper (11 x 17 inches). For teams
     outside North America, page size must be the closest size available to      10             10
     ANSI B. Plans must only consist of one (1) sheet and must have the
     US standard third-order projection.
  Required View
     The plans shall consist of a standard aeronautical three-view, using a
     US-standard third-order projection; i.e., right side view in the lower
                                                                                 10             10
     left with the nose pointing right, top view above the right side view
     also with the nose pointing right, and front view in the lower right.


  Dimensions
     Dimensions must be in inches and decimal inches, to an appropriate          10             10
     level of precision.
  Summary data
     The sheet containing the three-view must also contain a table with a
     summary of pertinent aircraft data such as wingspan, empty weight,          10             10
     engine make and model for Open Class or Micro Class, etc.


  Detail/Clarity
                                                                                 10             2
     School Name, Team Name, and Team Number on ALL pages




                                                     Page 3 of 12
                         SAE AERO-DESIGN REPORT GRADESHEET
                    Team 6 - University of Cincinnati (judge wh)
                                                                                               CLASS
                                                                                 Total      Regular Class
                                47.3                                              Points
                                                                                            Open Class
                                                                                Available
                                                                                            Micro Class

Prediction Graphs                                                                  50             40
   Number of Copies
     One copy of the payload prediction curve will be bound with each
     Design Report and will not count against the 30-page limit. One copy
     of the payload prediction curve will be provided loose-leaf, not bound        10             10
     to the reports. One copy per report times three reports plus one loose-
     leaf copy equals four payload prediction curves submitted.

  Paper Size
     Prediction curves must be printed on ANSI A sized paper (8 ½ x 11
     inches) in landscape format. For teams outside North America, paper           10             10
     size must be the closest size available to ANSI A.

  Graph Markings
     The payload prediction curve (graph) must be marked with the team
     name and school name across the top of the graph, and with the team           10             10
     number marked in the bottom-right corner. The graph must include
     the formula used to calculate the curve.

  Nature of Curve (See Section 60.1.3.4)
     The curve must present the payload capacity of the aircraft in pounds
     as a function of density altitude in feet. The graph must be linearized
     over the relevant range, and the linear equation used to predict the
     payload capacity must be clearly shown on the graph
     Only one curve, and hence one equation, may be presented on the
     graph. This curve may take into account predicted headwind for local
     conditions, rolling drag, inertia, engine and propeller performance, or
                                                                                   20             10
     any other factors that may affect takeoff performance. All these factors
     are allowed components of the prediction curve, but only one curve will
     be allowed; multiple curves to account for varying headwind conditions
     will not be allowed. Teams presenting multiple curves will receive no
     bonus points for payload prediction.




                                                     Page 4 of 12
                          SAE AERO-DESIGN REPORT GRADESHEET
                     Team 6 - University of Cincinnati (judge mj)
                                                                                           CLASS
                                                                             Total      Regular Class
                                   46.8                                       Points
                                                                                        Open Class
                                                                            Available
                                                                                        Micro Class

Design Report                                                                  400      Awarded Pts
 FORMAT & LAYOUT                                                               60           59
   Cover Page
     School Name
     Team Name                                                                 13             13
     Team Number
     Report Title
  Statement of Compliance (Page 2 of Report)
                                                                                5             5

  Table of Contents
                                                                                5             4
     Correct and accurate page references
  Format Requirements
     Paper Size
     Font (minimum size is 12 pts proportional or a 10 character per inch
     nonproportional font)                                                     12             12
     Margins
     Binding (No loose pages)
  Page Limit Requirement
     The report must not exceed (30) thirty double-space, typewritten          10             10
     pages including appendices.
  Three (3) copies of identical Design Report
                                                                               15             15

 DESIGN PROCESS                                                                160           153
  Introduction
     Definition of the Objective                                               30             28
     Requirement Statement
  Research
     Discussion of Concepts
                                                                               40             38
     Discussion of previous design/concepts/publications
     Test & Experiment (Method and Procedures)
  Design Analysis & Review Process
                                                                               45             43
     Discussion of Results
  Design Selection Process
                                                                               45             44
     Why certain design was selected over others

 CALCULATIONS                                                                  60             53
  Performance
                                                                               12             11
     Equations, Calculation, Charts, and/or Tables
  Stability & Control
                                                                               12             11
     Equations, Calculation, Charts, and/or Tables
  Aircraft Sizing
                                                                               12             10
     Equations, Calculation, Charts, and/or Tables
  Weight Build-up and Analysis
                                                                               12             11
     Equations, Calculation, Charts, and/or Tables
  Structural Analysis
     Equations, Calculation, Charts, and/or Tables
                                                                               12             10




                                                     Page 5 of 12
                     SAE AERO-DESIGN REPORT GRADESHEET
                Team 6 - University of Cincinnati (judge mj)
                                                                    CLASS
                                                      Total      Regular Class
                      46.8                             Points
                                                                 Open Class
                                                     Available
                                                                 Micro Class

INNOVATIONS                                             50             44
 Process/methods
                                                        10             8

 Design
                                                        10             9

 Application
                                                        10             10

 Construction
                                                        10             8

 Use of Computer Aided Design tools
                                                        10             9

WRITING                                                 70             66
 Spelling
                                                        10             10

 Grammar
                                                        10             10

 Sentence structure
                                                        10             10

 Punctuation
                                                        10             10

 Clarity
                                                        10             8

 Organization
                                                        10             9

 Accurate Table and Figure identifications
                                                        10             9




                                      Page 6 of 12
                         SAE AERO-DESIGN REPORT GRADESHEET
                    Team 6 - University of Cincinnati (judge mj)
                                                                                             CLASS
                                                                               Total      Regular Class
                                46.8                                            Points
                                                                                          Open Class
                                                                              Available
                                                                                          Micro Class

Plans                                                                            50             43
   Paper Size
     Plan sheet must be ANSI B sized paper (11 x 17 inches). For teams
     outside North America, page size must be the closest size available to      10             10
     ANSI B. Plans must only consist of one (1) sheet and must have the
     US standard third-order projection.
  Required View
     The plans shall consist of a standard aeronautical three-view, using a
     US-standard third-order projection; i.e., right side view in the lower
                                                                                 10             10
     left with the nose pointing right, top view above the right side view
     also with the nose pointing right, and front view in the lower right.


  Dimensions
     Dimensions must be in inches and decimal inches, to an appropriate          10             10
     level of precision.
  Summary data
     The sheet containing the three-view must also contain a table with a
     summary of pertinent aircraft data such as wingspan, empty weight,          10             8
     engine make and model for Open Class or Micro Class, etc.


  Detail/Clarity
                                                                                 10             5
     School Name, Team Name, and Team Number on ALL pages




                                                     Page 7 of 12
                         SAE AERO-DESIGN REPORT GRADESHEET
                    Team 6 - University of Cincinnati (judge mj)
                                                                                               CLASS
                                                                                 Total      Regular Class
                                46.8                                              Points
                                                                                            Open Class
                                                                                Available
                                                                                            Micro Class

Prediction Graphs                                                                  50             50
   Number of Copies
     One copy of the payload prediction curve will be bound with each
     Design Report and will not count against the 30-page limit. One copy
     of the payload prediction curve will be provided loose-leaf, not bound        10             10
     to the reports. One copy per report times three reports plus one loose-
     leaf copy equals four payload prediction curves submitted.

  Paper Size
     Prediction curves must be printed on ANSI A sized paper (8 ½ x 11
     inches) in landscape format. For teams outside North America, paper           10             10
     size must be the closest size available to ANSI A.

  Graph Markings
     The payload prediction curve (graph) must be marked with the team
     name and school name across the top of the graph, and with the team           10             10
     number marked in the bottom-right corner. The graph must include
     the formula used to calculate the curve.

  Nature of Curve (See Section 60.1.3.4)
     The curve must present the payload capacity of the aircraft in pounds
     as a function of density altitude in feet. The graph must be linearized
     over the relevant range, and the linear equation used to predict the
     payload capacity must be clearly shown on the graph
     Only one curve, and hence one equation, may be presented on the
     graph. This curve may take into account predicted headwind for local
     conditions, rolling drag, inertia, engine and propeller performance, or
                                                                                   20             20
     any other factors that may affect takeoff performance. All these factors
     are allowed components of the prediction curve, but only one curve will
     be allowed; multiple curves to account for varying headwind conditions
     will not be allowed. Teams presenting multiple curves will receive no
     bonus points for payload prediction.




                                                     Page 8 of 12
                          SAE AERO-DESIGN REPORT GRADESHEET
                     Team 6 - University of Cincinnati (judge lr)
                                                                                           CLASS
                                                                             Total      Regular Class
                                   48.4                                       Points
                                                                                        Open Class
                                                                            Available
                                                                                        Micro Class

Design Report                                                                  400      Awarded Pts
 FORMAT & LAYOUT                                                                60           59
   Cover Page
     School Name
     Team Name                                                                 13             13
     Team Number
     Report Title
  Statement of Compliance (Page 2 of Report)
                                                                                5             5

  Table of Contents
                                                                                5             4
     Correct and accurate page references
  Format Requirements
     Paper Size
     Font (minimum size is 12 pts proportional or a 10 character per inch
     nonproportional font)                                                     12             12
     Margins
     Binding (No loose pages)
  Page Limit Requirement
     The report must not exceed (30) thirty double-space, typewritten          10             10
     pages including appendices.
  Three (3) copies of identical Design Report
                                                                               15             15

 DESIGN PROCESS                                                                160           160
  Introduction
     Definition of the Objective                                               30             30
     Requirement Statement
  Research
     Discussion of Concepts
                                                                               40             40
     Discussion of previous design/concepts/publications
     Test & Experiment (Method and Procedures)
  Design Analysis & Review Process
                                                                               45             45
     Discussion of Results
  Design Selection Process
                                                                               45             45
     Why certain design was selected over others

 CALCULATIONS                                                                  60             45
  Performance
                                                                               12             9
     Equations, Calculation, Charts, and/or Tables
  Stability & Control
                                                                               12             9
     Equations, Calculation, Charts, and/or Tables
  Aircraft Sizing
                                                                               12             9
     Equations, Calculation, Charts, and/or Tables
  Weight Build-up and Analysis
                                                                               12             9
     Equations, Calculation, Charts, and/or Tables
  Structural Analysis
     Equations, Calculation, Charts, and/or Tables
                                                                               12             9




                                                     Page 9 of 12
                     SAE AERO-DESIGN REPORT GRADESHEET
                Team 6 - University of Cincinnati (judge lr)
                                                                     CLASS
                                                       Total      Regular Class
                      48.4                              Points
                                                                  Open Class
                                                      Available
                                                                  Micro Class

INNOVATIONS                                              50             50
 Process/methods
                                                         10             10

 Design
                                                         10             10

 Application
                                                         10             10

 Construction
                                                         10             10

 Use of Computer Aided Design tools
                                                         10             10

WRITING                                                  70             70
 Spelling
                                                         10             10

 Grammar
                                                         10             10

 Sentence structure
                                                         10             10

 Punctuation
                                                         10             10

 Clarity
                                                         10             10

 Organization
                                                         10             10

 Accurate Table and Figure identifications
                                                         10             10




                                      Page 10 of 12
                          SAE AERO-DESIGN REPORT GRADESHEET
                     Team 6 - University of Cincinnati (judge lr)
                                                                                             CLASS
                                                                               Total      Regular Class
                                48.4                                            Points
                                                                                          Open Class
                                                                              Available
                                                                                          Micro Class

Plans                                                                            50             50
   Paper Size
     Plan sheet must be ANSI B sized paper (11 x 17 inches). For teams
     outside North America, page size must be the closest size available to      10             10
     ANSI B. Plans must only consist of one (1) sheet and must have the
     US standard third-order projection.
  Required View
     The plans shall consist of a standard aeronautical three-view, using a
     US-standard third-order projection; i.e., right side view in the lower
                                                                                 10             10
     left with the nose pointing right, top view above the right side view
     also with the nose pointing right, and front view in the lower right.


  Dimensions
     Dimensions must be in inches and decimal inches, to an appropriate          10             10
     level of precision.
  Summary data
     The sheet containing the three-view must also contain a table with a
     summary of pertinent aircraft data such as wingspan, empty weight,          10             10
     engine make and model for Open Class or Micro Class, etc.


  Detail/Clarity
                                                                                 10             10
     School Name, Team Name, and Team Number on ALL pages




                                                    Page 11 of 12
                           SAE AERO-DESIGN REPORT GRADESHEET
                      Team 6 - University of Cincinnati (judge lr)
                                                                                                CLASS
                                                                                 Total       Regular Class
                                 48.4                                             Points
                                                                                             Open Class
                                                                                Available
                                                                                             Micro Class

Prediction Graphs                                                                  50              50
   Number of Copies
      One copy of the payload prediction curve will be bound with each
      Design Report and will not count against the 30-page limit. One copy
      of the payload prediction curve will be provided loose-leaf, not bound       10              10
      to the reports. One copy per report times three reports plus one loose-
      leaf copy equals four payload prediction curves submitted.

   Paper Size
      Prediction curves must be printed on ANSI A sized paper (8 ½ x 11
      inches) in landscape format. For teams outside North America, paper          10              10
      size must be the closest size available to ANSI A.

   Graph Markings
      The payload prediction curve (graph) must be marked with the team
      name and school name across the top of the graph, and with the team          10              10
      number marked in the bottom-right corner. The graph must include
      the formula used to calculate the curve.

   Nature of Curve (See Section 60.1.3.4)
      The curve must present the payload capacity of the aircraft in pounds
      as a function of density altitude in feet. The graph must be linearized
      over the relevant range, and the linear equation used to predict the
      payload capacity must be clearly shown on the graph
      Only one curve, and hence one equation, may be presented on the
      graph. This curve may take into account predicted headwind for local
      conditions, rolling drag, inertia, engine and propeller performance, or
                                                                                   20              20
      any other factors that may affect takeoff performance. All these
      factors are allowed components of the prediction curve, but only one
      curve will be allowed; multiple curves to account for varying headwind
      conditions will not be allowed. Teams presenting multiple curves will
      receive no bonus points for payload prediction.



 • Well written, good division of responsibilities, data
 • Some confusion on what the report was for, report was not stated it was for the regular
 class.
 • Need to clearly state purpose, goal and what you intend to do
 • Report should be easy to read, Use simple English, example: "problematic conundrum"
 does not help clarity
 • Explain / prove your analysis with data. example: "simple, complex, not accurate." need
 to quantify
 • Missing engine make, mode of class on 3 view sheet
 • School name, team & number needs to be on all sheets
 • Drawing on page 26 was not numbered
 • Need to summarize and state conclusions




                                                     Page 12 of 12

								
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