An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9 PDF Download
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Author: Michael C. Fischer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 76
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Book Description
Boundary layer transition on nose cones at hypersonic speeds.
Author: Michael C. Fischer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 76
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Book Description
Boundary layer transition on nose cones at hypersonic speeds.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 1004
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 92
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 816
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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.
Author: Charles Borden Johnson
Publisher:
ISBN:
Category : Reynolds number
Languages : en
Pages : 66
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Book Description
Author: O. L. Pearson
Publisher:
ISBN:
Category : Extravehicular space suits
Languages : en
Pages : 920
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Book Description
Simulated space environment performance tests of Apollo lunar module in thermal vacuum environment.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 256
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Book Description
Author: Thomas C. Corke
Publisher: Cambridge University Press
ISBN: 110896253X
Category : Technology & Engineering
Languages : en
Pages : 482
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Book Description
This book provides a comprehensive treatment of passive and active flow control in fluid dynamics, with an emphasis on utilizing fluid instabilities for enhancing control performance. Examples are given from a wide range of technologically important flow fields occurring in aerospace applications, from low-subsonic to hypersonic Mach numbers. This essential book can be used for both research and teaching on the topics of fluid instabilities, fluid measurement and flow actuator techniques, and problem sets are provided at the end of each chapter to reinforce key concepts and further extend readers' understanding of the field. The solutions manual is available as a online resource for instructors. The text is well suited for both graduate students in fluid dynamics and for practising engineers in the aerodynamics design field.
Author:
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ISBN:
Category : Research
Languages : en
Pages : 1318
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Book Description
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
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Book Description
