Numerical Investigation of the Laminar Boundary Layer on a 3-D Body Started Impulsively from Rest

Numerical Investigation of the Laminar Boundary Layer on a 3-D Body Started Impulsively from Rest

Author: U. Gulcat

Publisher:

Published: 1986

Total Pages: 6

ISBN-13:

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Unsteady flow of viscous incompressible fluid external to three dimensional bodies is considered. Based on the boundary layer concept the simplified version of the equations of motion are expressed in nonorthogonal coordinates which fits to body surface. The differential form of the equations are discretised with finite differencing to give a solution procedure which does not require any iteration discretised with finite differencing to give a solution procedure which does not require any iteration cylinder. The results obtained are compared with the experimental and the results of the previous numerical works available. Finally three dimensional impulsive flow past an oblate spheroid is considered. The metric coefficients and all the necessary geometrical features obtained analytically are used in the governing equations. The numerical solution is carried until the time of flow reversal that occurs at the rear stagnation point of the spheroid.


AGARD Advisory Report

AGARD Advisory Report

Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development

Publisher:

Published: 1987

Total Pages: 32

ISBN-13:

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Investigation of the Laminar Aerodynamic Heat-transfer Characteristics of a Hemisphere-cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8

Investigation of the Laminar Aerodynamic Heat-transfer Characteristics of a Hemisphere-cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8

Author: Davis H. Crawford

Publisher:

Published: 1956

Total Pages: 680

ISBN-13:

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At the stagnation point, the theory of Sibulkin, using the diameter and conditions behind the normal shock, was in good agreement with the experiment when the velocity graident at the stagnation opint appropriate to the free-stream Mach number was used.