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The Momentum Integral Approximation for Compressible Magnetogasdynamic Boundary-Layer Flow

Journal Article · · Journal of Applied Mechanics
DOI:https://doi.org/10.1115/1.3636523· OSTI ID:4695822
The drag of an adiabatic flat plate in an ionized gas for a constant magnetic field applied to the boundary layer on the plate is found by a momentum integral approximation of von Karman. Laminar, two-dimensional flow, zero pressure gradient, small magnetic Reynolds number, and negligible electrical conductivity outside the boundary layer are assumed. The solution is valid in particular to a continuous, perfect-gas plasma, of unitary Prandtl number, and for conditions when the interaction parameter is very small. The solution shows the following effects: the adiabatic wall temperature is independent of the magnetic field; there is an increase in the boundary-layer thickness as the magnetic-field strength is increased; and the viscous drag coefficient decreases whereas the coefficient of total drag increases. (auth)
Research Organization:
Univ. of Washington, Seattle
Sponsoring Organization:
USDOE
NSA Number:
NSA-17-028010
OSTI ID:
4695822
Journal Information:
Journal of Applied Mechanics, Journal Name: Journal of Applied Mechanics Journal Issue: 2 Vol. 30; ISSN 0021-8936; ISSN JAMCAV
Publisher:
ASME
Country of Publication:
Country unknown/Code not available
Language:
English

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