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Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75°
Language: en
Pages: 38

Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75°

Authors: Gerald V. Foster
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1960 - Publisher:

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Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75°
Language: en
Pages: 26

Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75°

Authors: M. Leroy Spearman
Categories: Airplanes
Type: BOOK - Published: 1959 - Publisher:

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Flight Stability and Automatic Control
Language: en
Pages: 464

Flight Stability and Automatic Control

Authors: Robert C. Nelson
Categories: History
Type: BOOK - Published: 1998 - Publisher:

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This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of c
Innovation in Flight
Language: en
Pages: 406

Innovation in Flight

Authors: Joseph R. Chambers
Categories: Aeronautics
Type: BOOK - Published: 2005 - Publisher:

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Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack-outer Wing Swept 75°and 108°
Language: en
Pages: 32

Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack-outer Wing Swept 75°and 108°

Authors: Ross B. Robinson
Categories: Aerodynamics
Type: BOOK - Published: 1960 - Publisher:

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