Experimental Data on Stagnation-point Gas Injection Cooling on a Hemisphere-cone in a Hypersonic Arc Tunnel PDF Download
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Author: John E. Grimaud
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
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Author: John E. Grimaud
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
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Author: Richard L. Humphrey
Publisher:
ISBN:
Category : Cooling
Languages : en
Pages : 60
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Tests were made with a cylindrical model transpiration cooled over a region plus or minus 15 deg. from the stagnation line. Air was used as the coolant. The model was tested at a nominal Mach number of 7.0. Wall temperatures and heat-transfer rates were in good agreement with predicted values. The effect of the external pressure distribution on the local coolant flow rate and wall temperature is discussed. (Author).
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 972
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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: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1812
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Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1152
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1156
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Author: C.W.P. Reuterswärd
Publisher: Springer Science & Business Media
ISBN: 3709180716
Category : Technology & Engineering
Languages : en
Pages : 729
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 466
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1150
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1036
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