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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

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

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

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

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

Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing

Edward J. Ray

Published: 1967

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 2.30 to 4.63 of a Supersonic Transport Model with a Variable-sweep M Wing

Published: 1965

Total Pages: 100

Stability Characteristics of a Variable-sweep Lightweight Fighter Configuration with a Keel-type Fuselage at Mach Numbers from 1.50 to 2.86

Published: 1967

Total Pages: 52

Transonic Longitudinal Aerodynamic Characteristics of a Variable-sweep Fighter Model Having Body-mounted Nacelles

Published: 1964

Total Pages: 54