Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Free-flight Investigation of Static Stability and Drag of Models of the Second and Third Stages of the Hemisphere-nosed X-17 at Mach Numbers from 4 to 10
Author: Free-flight Investigation of the Static Stability and Aerodynamic Drag of Three Blunt- Nosed Cylinder-flare Test Bodies at Mach Numbers from 13 to 17
Author: NASA Technical Note
Author: A Correlation Study of the Bow Wave Profiles of Blunt Bodies
Author: Alvin SeiffPublisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36
Book Description
An Exploratory Investigation of Fins as Stabilizers for Blunt-nosed Slender Bodies at Hypersonic Speeds
Author: Static Longitudinal Stability of a Blunt-nosed Cylinder with Flared Afterbody at a Mach Number of 19.2
Author: Static Longitudinal Stability of a Missile Configuration with Various Nose Shapes and Flared Afterbodies at a Mach Number of 6.82
Author: Jim A. PenlandThe Effect of the Bow Shock Wave on the Stability of Blunt-nosed Slender Bodies
Author: Alvin SeiffTechnical Abstract Bulletin
Author: Measurements of the Mach Number and Pressure on the Afterbody of a Blunt-nosed Model in Free Flight at Mach Numbers from 6.5 to 14
Author: Simon C. SommerPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
Book Description