Measurements of Mutual Interference Heating for a Probe Antenna Mounted on an Apollo Reentry Configuration PDF Download
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Author: Robert A. Jones
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
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Book Description
Author: Robert A. Jones
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
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Book Description
Author: UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION.
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
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Book Description
Author: Robert A. Jones
Publisher:
ISBN:
Category :
Languages : en
Pages : 86
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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
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
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Book Description
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 402
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1508
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Book Description
Author: Lawrence E. Putnam
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 28
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Author: J. Wayne Keyes
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 146
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Book Description
An analytical and experimental study is presented of the aerodynamic heating resulting from six types of shock interference patterns encountered in high speed flow. Centerline measurements of pressure and heat transfer distributions on basic bodies were obtained in four wind tunnels for Mach numbers from 6 to 20, specific heat ratios from 1.27 to 1.67, and free stream Reynolds numbers from 3 million to 25.6 million per meter. Peak heating and peak pressures up to 17 and 7.5 times stagnation values, respectively, were measured. In general, results obtained from semiempirical methods developed for each of the six types of interference agreed with the experimental peaks.
