Author: G. F. TELENIN
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
Unsteady Supersonic Flow Over a Cone with a Blunted Tip
Author: G. F. TELENIN
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Technical Translations
Author:
Publisher:
ISBN:
Category : Periodicals
Languages : en
Pages : 1178
Book Description
Publisher:
ISBN:
Category : Periodicals
Languages : en
Pages : 1178
Book Description
Unsteady Supersonic Flow Past a Circular Cone Pitching and Plunging in a Plane
Author: Henry Wing H. Kan
Publisher:
ISBN:
Category :
Languages : en
Pages : 192
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 192
Book Description
U.S. Government Research Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 172
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 172
Book Description
Three-dimensional Inviscid Flow about Supersonic Blunt Cones at Angle of Attack
Author: M. J. Abbett
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 126
Book Description
The solution for the steady three-dimensional inviscid flow about supersonic blunt cones at angle of attack is obtained by coupling a direct time-dependent solution for the subsonic portion of the shock layer with steady state numerical afterbody solution. An outline is given covering the coupling scheme and the use of the resulting Fortran computer code.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 126
Book Description
The solution for the steady three-dimensional inviscid flow about supersonic blunt cones at angle of attack is obtained by coupling a direct time-dependent solution for the subsonic portion of the shock layer with steady state numerical afterbody solution. An outline is given covering the coupling scheme and the use of the resulting Fortran computer code.
The Flow Around a Narrow Blunted Cone at High Supersonic Velocity
Author: Cherny, Gorimir G
Publisher:
ISBN:
Category :
Languages : en
Pages : 3
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 3
Book Description
Keywords Index to U.S. Government Technical Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160
Book Description
Selected Technical Reports
Author: United States. Federal Aviation Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 590
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 590
Book Description
Bibliography of Scientific and Industrial Reports
Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 658
Book Description
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 658
Book Description