Data from Flow-field Surveys Behind a Large-scale Thin Straight Wing of Aspect Ratio 3

Data from Flow-field Surveys Behind a Large-scale Thin Straight Wing of Aspect Ratio 3 PDF Author: William T. Evans
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 22

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Data from Flow-field Surveys Behind a Large-scale Thin Straight Wing of Aspect Ratio 3

Data from Flow-field Surveys Behind a Large-scale Thin Straight Wing of Aspect Ratio 3 PDF Author: William T. Evans
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22

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Data from Flow-field Surveys Behind a Large-scale Thin Straight Wing of Aspect Ratio 3

Data from Flow-field Surveys Behind a Large-scale Thin Straight Wing of Aspect Ratio 3 PDF Author: William T. Evans
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ISBN:
Category : Airplanes
Languages : en
Pages : 13

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Limited flow-field surveys were made behind a large-scale thin straight wing of aspect ratio 3, both alone and in combination with a body and vertical tail. The wing section was a modified double wedge, 4.2 percent thick. The surveys were made at geometric angles of attack from 8 to 30 degrees, at a free-stream dynamic pressure of 20 pounds per square foot. The Reynolds number, based on the mean aerodynamic chord of the wing, was approximately 8,500,000.

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 388

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NASA Technical Note

NASA Technical Note PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 56

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NACA Research Memorandum

NACA Research Memorandum PDF Author:
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 56

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1932

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Research Memorandum

Research Memorandum PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category :
Languages : en
Pages : 716

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Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
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Category : United States
Languages : en
Pages : 1366

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Large-scale Wind-tunnel Tests of a Subsonic Transport with Aft Engine Nacelles and High Tail

Large-scale Wind-tunnel Tests of a Subsonic Transport with Aft Engine Nacelles and High Tail PDF Author: Kiyoshi Aoyagi
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 52

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Stability and Control of Airplanes and Helicopters

Stability and Control of Airplanes and Helicopters PDF Author: Edward Seckel
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Category : Stability of airplanes
Languages : en
Pages : 532

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Stability and Control of Airplanes and Helicopters deals with aircraft flying qualities that determine the stability and control of airplanes and helicopters. It includes problems based on real aircraft, selected to represent the gamut from simple to complicated, and from conventional utility designs to futuristic research types. Many of these problems involve comparison of theory and experiment to demonstrate their mutual relationship.