Handbook of Supersonic Aerodynamics PDF Download
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Author: D. Adamson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 366
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Book Description
Author: D. Adamson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 366
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Book Description
Author: Johns Hopkins University. Applied Physics Laboratory
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 102
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Book Description
Author: George Rudinger
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 452
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Book Description
Author: John A. Darling
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 170
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Book Description
The report describes methods for quickly estimating the normal force and center of pressure of blunt free-fall shapes of l/d = 0.5 to 10 over a Mach number range of 0.4 to 2.5 and up to alpha = 90 degrees. Charts and equations presented in the report are from cited reference material and original sources. Methods based on slender-body theory tested on blunt shapes and modifying factors were developed where needed.
Author: Russell M. Cummings
Publisher: Cambridge University Press
ISBN: 1107053749
Category : Mathematics
Languages : en
Pages : 893
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Book Description
This book covers the application of computational fluid dynamics from low-speed to high-speed flows, especially for use in aerospace applications.
Author: John A. Darling
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 72
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Book Description
Axial forces were measured on five cylinders at M = 5 for Re = 4,000,000/ft and 37,000,000/ft. The purpose of these tests was to measure the surface drag of the cylinders for various surface protrusion patterns. Using these experimental measurements and data from J.C. Westkaemper, an expression was developed for calculating the average effective drag coefficient of one protrusion in a row of protrusions which are fully submerged in a turbulent boundary layer. (Author).
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 886
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Book Description
Author: David L. Merritt
Publisher:
ISBN:
Category : Aerospace telemetry
Languages : en
Pages : 72
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Book Description
The ability of the Miniature Telemetry System to measure transient pressures on a model flying through a shock wave was investigated in the NOL Shock Interaction Range. Ten instrumented models were flown. (Author).
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 684
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Book Description
Author: Edward E. Mayo
Publisher:
ISBN:
Category : Newtonian cosmology
Languages : en
Pages : 36
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Book Description
