Measurement of the Pressure Distribution on Swept-back Wings with Trailing Edge Split Flaps

Measurement of the Pressure Distribution on Swept-back Wings with Trailing Edge Split Flaps PDF Author: College of Aeronautics (Cranfield, Bedfordshire)
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Languages : en
Pages : 24

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Measurement of the Pressure Distribution on Swept-back Wings with Trailing Edge Split Flaps

Measurement of the Pressure Distribution on Swept-back Wings with Trailing Edge Split Flaps PDF Author: College of Aeronautics (Cranfield, Bedfordshire)
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ISBN:
Category :
Languages : en
Pages : 24

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Measurements of the Pressure Distribution on Swept Back Wings with Trailing Edge Split Flaps

Measurements of the Pressure Distribution on Swept Back Wings with Trailing Edge Split Flaps PDF Author: Arthur William Babister
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Languages : en
Pages : 12

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Report

Report PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 160

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Index of NACA Technical Publications

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

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Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages :

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Report

Report PDF Author:
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Category : Aeronautics
Languages : en
Pages : 1180

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Determination of Longitudinal Stability and Control Characteristics from Free-flight Model Tests with Results at Transonic Speeds for Three Airplane Configurations

Determination of Longitudinal Stability and Control Characteristics from Free-flight Model Tests with Results at Transonic Speeds for Three Airplane Configurations PDF Author: Clarence L. Gills
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Category : Aeronautics
Languages : en
Pages : 442

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Pressure-distribution Measurements Over an Extensible Leading-edge Flap on Two Wings Having Leading-edge Sweep of 42 Degree and 52 Degree

Pressure-distribution Measurements Over an Extensible Leading-edge Flap on Two Wings Having Leading-edge Sweep of 42 Degree and 52 Degree PDF Author: Reino J. Salmi
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Category :
Languages : en
Pages : 36

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
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Category : Aeronautics
Languages : en
Pages : 750

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U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
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Category : Science
Languages : en
Pages : 144

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