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Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-sweep Fighter Model with Wing Sweep of 50 Deg, 60 Deg, and 75 Deg

Published: 1964

Total Pages: 38

Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.20 of a Variable Sweep Fighter Model with Wing Sweep Angles from 25 Deg to 75 Deg

Published: 1962

Total Pages: 28

Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Variablesweep Model at Sweep Angles from 55 Deg to 75 Deg

Published: 1964

Total Pages: 46

The Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.20 of a Variable-sweep Fighter Model with Wing Sweeps Varying from 25 Deg to 75 Deg

Published: 1963

Total Pages: 84

Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design

Odell A. Morris

Published: 1961

Total Pages: 32

Aerodynamic Characteristics at Mach Numbers from 1.60 to 4.63 of a Variable-sweep Fighter Model with Wing Sweep Angles of 44° and 71°

Milton Lamb

Published: 1972

Total Pages: 0

Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack - Outer Wing Swept 75 Deg

Published: 1960

Total Pages: 24

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 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

Transonic Aerodynamic Characteristics of a Variable-sweep Airplane Configuration Having a 12-percent-thick Wing and an Inboard Pivot Location

Ralph P. Bielat

Published: 1960

Total Pages: 84