Prediction of Normal Force, Pitching Moment, and Yawing Force on Bodies of Revolution at Angles of Attack Up to 50 Degrees Using a Concentrated Vortex Flow-field Model

Prediction of Normal Force, Pitching Moment, and Yawing Force on Bodies of Revolution at Angles of Attack Up to 50 Degrees Using a Concentrated Vortex Flow-field Model
Author: Andrew B. Wardlaw (Jr.)
Publisher:
Total Pages: 100
Release: 1973
Genre: Angle of attack (Aerodynamics)
ISBN:

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A method initially proposed by Bryson is extended to include asymmetric shedding. This method employs the impulsive flow analogy, and models each wake vortex using a single-point vortex. Free parameters inherent in the problem formulation are determined empirically. Normal force, pitching moment and yawing force coefficients are predicted for slender bodies with a nose fineness ratio greater than four and at a Mach number less than 0.9. (Modified author abstract).


Prediction of Normal Force, Pitching Moment, and Yawing Force on Bodies of Revolution at Angles of Attack Up to 50 Degrees Using a Concentrated Vortex Flow-field Model
Language: en
Pages: 100
Authors: Andrew B. Wardlaw (Jr.)
Categories: Angle of attack (Aerodynamics)
Type: BOOK - Published: 1973 - Publisher:

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A method initially proposed by Bryson is extended to include asymmetric shedding. This method employs the impulsive flow analogy, and models each wake vortex us
Prediction of Normal Force, Pitching Moment, and Yawing Force on Bodies of Revolution at Angles of Attack Up to 50 Degrees Using a Concentrated Vortex Flow-Field Model
Language: en
Pages: 94
Authors:
Categories:
Type: BOOK - Published: 1973 - Publisher:

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A method initially proposed by Bryson is extended to include asymmetric shedding. This method employs the impulsive flow analogy, and models each wake vortex us
Induced Side Forces on Bodies of Revolution at High Angle of Attack
Language: en
Pages: 52
Authors: Wardlaw, Jr. (Andrew B.)
Categories: Aerodynamic load
Type: BOOK - Published: 1975 - Publisher:

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Linear regression techniques are used to establish a quantitative description of side forces on bodies at high incidence. A data base is assembled concerning th
Naval Research Reviews
Language: en
Pages: 520
Authors:
Categories: Naval research
Type: BOOK - Published: 1976 - Publisher:

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Scientific and Technical Aerospace Reports
Language: en
Pages: 202
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1974 - Publisher:

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