Author: Frank W. Spaid
Publisher:
ISBN:
Category :
Languages : en
Pages : 116
Book Description
Experimental Results for a Hypersonic Nozzle/afterbody Flow Field
Scientific and Technical Aerospace Reports
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1112
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1112
Book Description
Research Review
Author: United States. Air Force. Office of Aerospace Research
Publisher:
ISBN:
Category :
Languages : en
Pages : 682
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 682
Book Description
Air Force Research Resumés
Technical Abstract Bulletin
Plasma Physics and Magnetohydrodynamics
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Magnetohydrodynamics
Languages : en
Pages : 290
Book Description
Publisher:
ISBN:
Category : Magnetohydrodynamics
Languages : en
Pages : 290
Book Description
Theories and Technologies of Hypervelocity Shock Tunnels
Author: Zonglin Jiang
Publisher: Cambridge University Press
ISBN: 1009035673
Category : Technology & Engineering
Languages : en
Pages : 316
Book Description
Introducing the state-of-the-art of hypervelocity shock tunnels, this complete reference features a variety of drivers and step-by-step introductions to their theories, physics, methods and testing. This book enables researchers and engineers in aerospace to design and improve wind tunnels that simulate flow qualities of real hypersonic flyers.
Publisher: Cambridge University Press
ISBN: 1009035673
Category : Technology & Engineering
Languages : en
Pages : 316
Book Description
Introducing the state-of-the-art of hypervelocity shock tunnels, this complete reference features a variety of drivers and step-by-step introductions to their theories, physics, methods and testing. This book enables researchers and engineers in aerospace to design and improve wind tunnels that simulate flow qualities of real hypersonic flyers.