An Experimental Investigation Of Boundary Layer Transition On A 10 Half Angle Cone At Mach 69
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Author | : Michael C. Fischer |
Publisher | : |
Total Pages | : 76 |
Release | : 1970 |
Genre | : Aerodynamics |
ISBN | : |
Boundary layer transition on nose cones at hypersonic speeds.
Author | : |
Publisher | : |
Total Pages | : 1004 |
Release | : 1970 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 816 |
Release | : 1989 |
Genre | : Aeronautics |
ISBN | : |
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 | : |
Publisher | : |
Total Pages | : 92 |
Release | : 1971 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 966 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 962 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
Author | : O. L. Pearson |
Publisher | : |
Total Pages | : 920 |
Release | : 1970 |
Genre | : Extravehicular space suits |
ISBN | : |
Simulated space environment performance tests of Apollo lunar module in thermal vacuum environment.
Author | : Thomas C. Corke |
Publisher | : Cambridge University Press |
Total Pages | : 482 |
Release | : 2024-04-11 |
Genre | : Technology & Engineering |
ISBN | : 110896253X |
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 | : |
Publisher | : |
Total Pages | : 172 |
Release | : 1970 |
Genre | : Dissertations, Academic |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 942 |
Release | : 1969 |
Genre | : Nuclear science abstracts |
ISBN | : |