An Experimental Investigation Using a Normal Jet Plume Simulator to Determine Jet Plume Effects on a Long Slender Rocket Configuration at Mach Numbers from 0.2 to 1.5 PDF Download
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Author: James H Henderson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 148
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Book Description
Experimental aerodynamic investigations were conducted at the AEDC 16-foot Transonic Wind Tunnel to determine longitudinal stability characteristics of a long slender rocket configuration with simulated jet plume. The effect of jet plume on rocket aerodynamics is given over an angle of attack range from -11 to 11 degrees at Mach numbers from 0.2 to 1.5. Plume simulator chamber pressure varied from 0 to 600 psia. Individual cruciform fin aerodynamic loads are also shown over the same ranges. (Author).
Author: James H Henderson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 148
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Book Description
Experimental aerodynamic investigations were conducted at the AEDC 16-foot Transonic Wind Tunnel to determine longitudinal stability characteristics of a long slender rocket configuration with simulated jet plume. The effect of jet plume on rocket aerodynamics is given over an angle of attack range from -11 to 11 degrees at Mach numbers from 0.2 to 1.5. Plume simulator chamber pressure varied from 0 to 600 psia. Individual cruciform fin aerodynamic loads are also shown over the same ranges. (Author).
Author:
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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:
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Category :
Languages : en
Pages : 864
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 1076
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 484
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Author:
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Category :
Languages : en
Pages : 444
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Author: Robert J. Krieger
Publisher:
ISBN:
Category : Cruise missiles
Languages : en
Pages : 136
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Book Description
This report presents the results of a program that investigated aerodynamic configuring as a method of improving long range supersonic cruise and maneuvering missile performance. Non-circular body, lifting body, blended wing body, wing-body and favorable interference concepts were developed and wind tunnel tested. Substantial improvements in cruise range were shown to result from aero configuring.
Author:
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Category : Aeronautics
Languages : en
Pages : 1102
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Author:
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ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 948
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Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 880
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