Application of Dorodnitsyn's Integral Method to Nonequilibrium Flows Over Pointed Bodies

Application of Dorodnitsyn's Integral Method to Nonequilibrium Flows Over Pointed Bodies PDF Author: Jerry Curtis South
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56

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Application of Dorodnitsyn's Integral Method to Nonequilibrium Flows Over Pointed Bodies

Application of Dorodnitsyn's Integral Method to Nonequilibrium Flows Over Pointed Bodies PDF Author: Jerry Curtis South
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 482

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Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners

Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners PDF Author: Jerry Curtis South
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ISBN:
Category : Mathematical models
Languages : en
Pages : 66

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Application of a One-strip Integral Method to the Unsteady Supersonic Aerodynamics of an Inclined Flat Surface

Application of a One-strip Integral Method to the Unsteady Supersonic Aerodynamics of an Inclined Flat Surface PDF Author: Robert M. Bennett
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 68

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The method of integral relations is applied in a one-strip approximation to the perturbation equations governing small motions of an inclined, sharp-edged, flat surface about the mean supersonic steady flow. Algebraic expressions for low reduced-frequency aerodynamics are obtained and a set of ordinary differential equations are obtained for general oscillatory motion. Results are presented for low reduced-frequency aerodynamics and for the variation of the unsteady forces with frequency. The method gives accurate results for the aerodynamic forces at low reduced frequency which are in good agreement with available experimental data. However, for cases in which the aerodynamic forces vary rapidly with frequency, the results are qualitatively correct, but of limited accuracy. Calculations indicate that for a range of inclination angles near shock detachment such that the flow in the shock layer is low supersonic, the aerodynamic forces vary rapidly both with inclination angle and with reduced frequency.

ARL [report]

ARL [report] PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 124

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1196

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 356

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Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
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ISBN:
Category : United States
Languages : en
Pages : 1250

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 262

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258

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