Comparison of Experimental and Theoretical Shock Shapes and Pressure Distributions on Flat-faced Cylinders at Mach 10.5 PDF Download
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Author: Mamoru Inouye
Publisher:
ISBN:
Category : Cylinder (Mathematics)
Languages : en
Pages : 26
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Book Description
Author: Mamoru Inouye
Publisher:
ISBN:
Category : Cylinder (Mathematics)
Languages : en
Pages : 26
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Book Description
Author: Mamoru Inouye
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 732
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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: A. B. Bailey
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 72
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Book Description
An experimental investigation was made to determine the pressure distribution, shock shape, and shock detachment distance for spheres and the latter two characteristics for flatfaced bodies in a heated argon flow. The modified Newtonian approximation for the pressure distribution, which is strictly an empirical relationship, gives good results when applied to the first 60 degrees of a hemisphere under conditions where the body boundary layer and the shock layer merge. The natural flow visualization produced as a result of the high total temperature and consequent excitation of the argon enabled this study to be made. Photographs taken of the shocks generated by a series of spheres and flat-faced bodies were analyzed with a photo-densitometer to determine the shock shape and shock detachment distance. The blast analogy predicts a difference in the shape of shocks in argon and air at high Mach numbers and Reynolds numbers. An empirical relationship proposed by Love was used to calculate the shock shape in air for Mach numbers corresponding to those of the present investigation. (Author).
Author: Edward W. Perkins
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 50
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Book Description
Normal-force and pressure distributions have been determined for a body of revolution consisting of a fineness-ratio-3, circular-arc, ogival nose tangent to a cylindrical afterbody 7 diameters long. The free-stream Mach number was 1.98; the angle-of-attack range was from 0 to 20 degrees; and the Reynolds numbers, based on body diameter, were 150,000 and 450,000.
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 700
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Author: Raymond H. Eaves
Publisher:
ISBN:
Category :
Languages : en
Pages : 59
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Author: Lawrence Eugene Tisserand
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
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Author: William C. Morgan
Publisher:
ISBN:
Category : Elasticity
Languages : en
Pages : 26
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Author: Frank J. Centolanzi
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 82
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