(PDF) e-Book Aerodynamic Characteristics Of A Flat Bottom Canted Nose Half Cone Reentry Configuration At A Mach Number Of 67 Full Download

Download Free Aerodynamic Characteristics Of A Flat Bottom Canted Nose Half Cone Reentry Configuration At A Mach Number Of 67 Book in PDF and EPUB Free Download. You can read online Aerodynamic Characteristics Of A Flat Bottom Canted Nose Half Cone Reentry Configuration At A Mach Number Of 67 and write the review.

Aerodynamic Characteristics of a Flat-bottom Canted-nose Half-cone Reentry Configuration at a Mach Number of 6.7

William O. Armstrong

Published: 1962

Total Pages: 44

Pressure Distribution on a Flat-bottom Canted Nose Half-cone Reentry Configuration at a Mach Number of 6.0

Published: 1962

Total Pages: 28

The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90

George C. Kenyon

Published: 1961

Total Pages: 54

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

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

THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92

Published: 1961

Total Pages: 68

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

The Longitudinal Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half-cone at Mach Numbers to 0.92

George C. Kenyon

Published: 1961

Total Pages: 63

The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90

Published: 1961

Total Pages: 54

Aerodynamic Characteristics of a Modified Cone

George C. Ashby

Published: 1968

Total Pages: 26