Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1264
Book Description
OAR Cumulative Index of Research Results
Scientific and Technical Aerospace Reports
Technical Abstract Bulletin
Applied Mechanics Reviews
U.S. Government Research & Development Reports
Government-wide Index to Federal Research & Development Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1352
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1352
Book Description
OAR Research Review
Author: United States. Air Force. Office of Aerospace Research
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 528
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 528
Book Description
Research Review
Author: United States. Air Force. Office of Aerospace Research
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 368
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 368
Book Description
Bibliography of Scientific and Industrial Reports
The Effect of Severe Nose Bluntness on the Stability of Slender Cones in Hypersonic Flow
Author: Brian Quinn
Publisher:
ISBN:
Category : Noses (Space vehicles).
Languages : en
Pages : 0
Book Description
The flow around a blunted slender cone performing pitching oscillations is theoretically analyzed by means of Chernyi's blast-wave piston analogy. Stationary and transient shock shapes and pressure distributions are presented in power series form. Within the region of applicability, the stationary pressure agrees well with Chernyi's numerical integration. Normal force and pitching moment coefficient derivatives are presented and the results are plotted for a 10 degree cone. The theoretical static and dynamic stability derivatives agree satisfactorily with recent experiments in a Mach 14 wind tunnel. It is concluded that the experimentally observed reduction in static and dynamic stability due to increased nose bluntness may be attributed to blast wave effects. (Author).
Publisher:
ISBN:
Category : Noses (Space vehicles).
Languages : en
Pages : 0
Book Description
The flow around a blunted slender cone performing pitching oscillations is theoretically analyzed by means of Chernyi's blast-wave piston analogy. Stationary and transient shock shapes and pressure distributions are presented in power series form. Within the region of applicability, the stationary pressure agrees well with Chernyi's numerical integration. Normal force and pitching moment coefficient derivatives are presented and the results are plotted for a 10 degree cone. The theoretical static and dynamic stability derivatives agree satisfactorily with recent experiments in a Mach 14 wind tunnel. It is concluded that the experimentally observed reduction in static and dynamic stability due to increased nose bluntness may be attributed to blast wave effects. (Author).