Dynamic Directional Stability Derivatives for a 45 Degree Swept-wing-vertical-tail Airplane Model at Transonic Speeds and Angles of Attack, with a Description of the Mechanism and Instrumentation Employed

Dynamic Directional Stability Derivatives for a 45 Degree Swept-wing-vertical-tail Airplane Model at Transonic Speeds and Angles of Attack, with a Description of the Mechanism and Instrumentation Employed
Author: Albert L. Braslow
Publisher:
Total Pages: 46
Release: 1958
Genre:
ISBN:

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NASA Technical Note

NASA Technical Note
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 940
Release: 1959
Genre:
ISBN:

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Index of NASA Technical Publications

Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 448
Release: 1960
Genre: Aeronautics
ISBN:

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Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 388
Release: 1959
Genre: Aeronautics
ISBN:

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NASA Technical Memorandum

NASA Technical Memorandum
Author:
Publisher:
Total Pages: 592
Release: 1959
Genre: Aeronautics
ISBN:

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Index to NASA Technical Publications

Index to NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 208
Release: 1959
Genre:
ISBN:

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The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing

The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing
Author: Donald E. Hewes
Publisher:
Total Pages: 36
Release: 1951
Genre: Airplanes
ISBN:

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The trends in lateral stability and control produced variations of the mass distribution were determined for a model with a 45 degree sweptback wing. Calculations were made to correlate the trends determined by theory with those determined from tests of a free-flying dynamic model in the Langley free-flight tunnel.