Viscous Hypersonic Flow Over Pointed Cones at Low Reynolds Numbers
Author : H. F. Waldron
Publisher :
Page : 90 pages
File Size : 31,79 MB
Release : 1966
Category : Aerodynamics, Hypersonic
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Author : H. F. Waldron
Publisher :
Page : 90 pages
File Size : 31,79 MB
Release : 1966
Category : Aerodynamics, Hypersonic
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Author :
Publisher :
Page : 836 pages
File Size : 14,43 MB
Release : 1994
Category : Aeronautics
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Author : Max Kinslow
Publisher :
Page : 78 pages
File Size : 34,49 MB
Release : 1974
Category : Cone
ISBN :
The static pressure distribution on sharp and blunt 10-deg half-angle cones was measured under rarefied conditions in both a uniform and a source flow field. Angle of attack of the cones was varied up to 10 deg. Pressure distributions are presented for cold-wall conditions at 18.0 = or
Author :
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Page : 528 pages
File Size : 39,74 MB
Release : 1970
Category :
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Author :
Publisher :
Page : 184 pages
File Size : 19,42 MB
Release : 1984
Category : Astronautics
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Author :
Publisher :
Page : 988 pages
File Size : 12,74 MB
Release : 1973
Category : Science
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Author : United States. Air Force. Office of Aerospace Research
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Page : 586 pages
File Size : 41,48 MB
Release : 1965
Category : Aeronautics
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Author : Zhi-Hui Wang
Publisher : Springer
Page : 107 pages
File Size : 25,75 MB
Release : 2014-08-28
Category : Technology & Engineering
ISBN : 3662443651
Theoretical Modelling of Aeroheating on Sharpened Noses under Rarefied Gas Effects and Nonequilibrium Real Gas Effects employs a theoretical modeling method to study hypersonic flows and aeroheating on sharpened noses under rarefied gas effects and nonequilibrium real gas effects that are beyond the scope of traditional fluid mechanics. It reveals the nonlinear and nonequilibrium features, discusses the corresponding flow and heat transfer mechanisms, and ultimately establishes an analytical engineering theory framework for hypersonic rarefied and chemical nonequilibrium flows. The original analytical findings presented are not only of great academic significance, but also hold considerable potential for applications in engineering practice. The study explores a viable new approach, beyond the heavily relied-upon numerical methods and empirical formulas, to the present research field, which could be regarded as a successful implementation of the idea and methodology of the engineering sciences.
Author : Cornell Aeronautical Laboratory
Publisher :
Page : 320 pages
File Size : 35,49 MB
Release : 1967
Category : Gas flow
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Author :
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Page : 592 pages
File Size : 39,2 MB
Release :
Category : Military research
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