Roll-damping Derivative Calculations for Spinning Sharp and Blunt Cones in Supersonic and Hypersonic Flow PDF Download
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Author: Arloe W. Mayne (Jr.)
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 28
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Book Description
The boundary-layer equations in a Crocco variables form have been numerically solved for flow over spinning sharp and blunt cones at zero incidence to supersonic and hypersonic streams. Both laminar and turbulent flows have been treated, and for the blunt cases swallowing of the inviscid entropy layer by the boundary layer has been considered. The item of primary interest is roll damping, and results of a parametric study involving Mach number, Reynolds number, cone angle, and bluntness ratio are presented. Limited comparisons with experimental data and another method of computation are also presented. (Author).
Author: Arloe W. Mayne (Jr.)
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 28
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Book Description
The boundary-layer equations in a Crocco variables form have been numerically solved for flow over spinning sharp and blunt cones at zero incidence to supersonic and hypersonic streams. Both laminar and turbulent flows have been treated, and for the blunt cases swallowing of the inviscid entropy layer by the boundary layer has been considered. The item of primary interest is roll damping, and results of a parametric study involving Mach number, Reynolds number, cone angle, and bluntness ratio are presented. Limited comparisons with experimental data and another method of computation are also presented. (Author).
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 738
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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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ISBN:
Category : Science
Languages : en
Pages : 1048
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 1414
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1264
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Author:
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ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 938
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Author: Steven R. Vukelich
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 310
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Book Description
This report summarizes the methods available to predict the aerodynamic static, dynamic, and control characteristics of missiles. The methods selected for Missile Datcom development were based upon a criteria which included ease of use, accuracy, utility over a range of flight conditions and cost effective in their use. This report describes the methodology appropriate for the missile designer. An outline of a Missile Datcom handbook is proposed; an automated version is also recommended for development. Those areas presently lacking suitable methodologies are also highlighted. (Author).
Author: United States. Air Force. Office of Aerospace Research
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ISBN:
Category :
Languages : en
Pages : 1262
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 914
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