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Aerodynamic Characteristics at a Mach Number of 6.77 of a 9 ̊cone Configuration, with and Without Spherical Afterbodies, at Angles of Attack Up to 180 ̊with Various Degrees of Nose Blunting

Luther Neal (Jr.)

Published: 1963

Total Pages: 32

Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium

Melvin J. Fohrman

Published: 1963

Total Pages: 48

Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300

Jim A. Penland

Published: 1961

Total Pages: 50

Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85

Lucille C. Coltrane

Published: 1962

Total Pages: 32

A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp-and Blunt-nose Cones Having Flat and Modified Bases

Sandia Corporation

Published: 1965

Total Pages: 596

Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180°

Leroy Devan

Published: 1980

Total Pages: 192

Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares

A. B. Carraway

Published: 1960

Total Pages: 124

Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects

Dal V. Maddalon

Published: 1966

Total Pages: 42

Aerodynamic Characteristics of a Modified Cone

George C. Ashby

Published: 1968

Total Pages: 26

Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds

K. R. Czarnecki

Published: 1961

Total Pages: 36