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Lab 8 Basic Airplane Configuration Design-Design Analysis And Aeronautical Engineering-Lab Handout, Exercises of Aeronautical Engineering

This is lab report and manual for Design Analysis and Aeronautical Engineering course lab. It was submitted to Dr. Aadhunik Joshi at Bidhan Chandra Krishi Viswa Vidyalaya. It includes: Basic, Airplane, Configuration, Design, Tail, Surfaces, Dihedral, Stability, Control, Criteria, Layout

Typology: Exercises

2011/2012

Uploaded on 07/22/2012

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Lab 8 Basic Airplane Configuration Design
Unified Engineering
6 Apr 06
Learning Ob jectives
Sizing of tail surfaces and dihedral to meet stability and control criteria.
Design of aircraft layout.
3-View and table documentation of aircraft configuration.
Procedure
Correct any calculation errors which occurred in the wing design in La b 7.
Choose a specific wing design. This may differ somewhat from what you submitted for
Lab 7, even if that was correct.
Optional “field research”: Measure Plane Vanilla, and compute its stability and control
parameters: S.M., Vh, Vv, B
Choose suitable stability and control parameter values for your airplane, and design an
aircraft configuration to match. This will involve selecting AR h, S h, S v, h, stylish tail sur-
face planforms, etc. Iterate if necessary. Sketching a top-view of the airplane during this
procedure may be helpful. Determine the NP and CG locations for your airplane.
Draw a dimensionally-accurate 3-view. Draw and label the NP and CG locations on the
side view and/or top view. It’s traditional to also add a summary table of key airplane
info to the 3-view drawing: Catchy name, S , b , W , motor, battery. Also include your team
number on the 3-view, so it’s a stand-alone do cument.
Also make up a separate and more complete table of all the significant parameters describ-
ing your airplane: b , S , AR , W , λ , τ , CDA 0, S.M., Vh, etc. This table must also include the
key performance parameters: P min, V m ax, t . Include your team number in the table caption,
so it’s a stand-alone document.
Reporting
Each team will turn in one report.
Contents:
Title, team number, team member names, date.
Brief introduction explaining purpose of the report, aimed at an outside reader.
Briefly explain any fixes and/or design changes made since Lab 7.
Table of stability and control parameter values that you chose for your airplane. One or
two sentences explaining how you arrived at each choice.
3-view of your airplane. A neat pencil drawing is perfectly adequate, but in this case you
should submit a printed scan or a Xerox copy (save your original in a safe place).
Parameter table for your airplane.
Each team should maintain an up-to-date 3-view and parameter table for the remainder of
the term. You will be required to re-submit updated versions of these for each of the next
several labs, even if no changes were made.
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Lab 8 – Basic Airplane Configuration Design

Unified Engineering

6 Apr 06

Learning Objectives

  • Sizing of tail surfaces and dihedral to meet stability and control criteria.
  • Design of aircraft layout.
  • 3-View and table documentation of aircraft configuration.

Procedure

  • Correct any calculation errors which occurred in the wing design in Lab 7.
  • Choose a specific wing design. This may differ somewhat from what you submitted for Lab 7, even if that was correct.
  • Optional “field research”: Measure Plane Vanilla, and compute its stability and control parameters: S.M., Vh, Vv, B
  • Choose suitable stability and control parameter values for your airplane, and design an aircraft configuration to match. This will involve selecting ARh, Sh, Sv, ℓh, stylish tail sur- face planforms, etc. Iterate if necessary. Sketching a top-view of the airplane during this procedure may be helpful. Determine the NP and CG locations for your airplane.
  • Draw a dimensionally-accurate 3-view. Draw and label the NP and CG locations on the side view and/or top view. It’s traditional to also add a summary table of key airplane info to the 3-view drawing: Catchy name, S , b, W , motor, battery. Also include your team number on the 3-view, so it’s a stand-alone document.
  • Also make up a separate and more complete table of all the significant parameters describ- ing your airplane: b, S , AR, W , λ, τ , CDA 0 , S.M., Vh, etc. This table must also include the key performance parameters: Pmin, Vmax, t. Include your team number in the table caption, so it’s a stand-alone document.

Reporting

  • Each team will turn in one report.
  • Contents: — Title, team number, team member names, date. — Brief introduction explaining purpose of the report, aimed at an outside reader. — Briefly explain any fixes and/or design changes made since Lab 7. — Table of stability and control parameter values that you chose for your airplane. One or two sentences explaining how you arrived at each choice. — 3-view of your airplane. A neat pencil drawing is perfectly adequate, but in this case you should submit a printed scan or a Xerox copy (save your original in a safe place). — Parameter table for your airplane.

Each team should maintain an up-to-date 3-view and parameter table for the remainder of the term. You will be required to re-submit updated versions of these for each of the next several labs, even if no changes were made.

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