(PDF) e-Book Stability And Control Characteristics At Mach Numbers Of 250 300 And 371 Of A Variable Wing Sweep Configuration With Outboard Wing Panels Swept Back 75 Full Download

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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°

Gerald V. Foster

Published: 1960

Total Pages: 38

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

M. Leroy Spearman

Published: 1959

Total Pages: 26

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 Deg

Published: 1960

Total Pages: 38

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

Published: 1959

Total Pages: 22

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

M. Leroy Spearman

Published: 1959

Total Pages: 18

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°

Ross B. Robinson

Published: 1960

Total 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 Deg and 108 Deg

Published: 1960

Total Pages: 28

Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable- Sweep Wings

Published: 1960

Total Pages: 48

Stability and Control Characteristics at a Mach Number of 2.2 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack - Outer Wing Swept 75 Deg

Published: 1960

Total Pages: 28

Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-sweep Wings

Bernard Spencer

Published: 1960

Total Pages: 98