On fully developed channel flows: some solutions and limitations, and effects of compressibility, variable properties, and body forces
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Maslen, Stephen H↗
Engineering topics
Maslen, Stephen H
Publications and source records attributed to Maslen, Stephen H.
Transverse oscillations in a cylindrical combustion chamber
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Moore, Franklin K↗
Second approximation to laminar compressible boundary layer on flat plate in slip flow
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Maslen, Stephen H↗
Three-dimensional supersonic nozzles and inlets of arbitrary exit cross section
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Evvard, John C↗
Supersonic conical flow
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Maslen, Stephen H↗
Experimental Pressure Distributions over Two Wing-body Combinations at Mach Number 1.9
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Moskowitz, Barry↗
Turbulent boundary-layer temperature recovery factors in two-dimensional supersonic flow
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BOUNDARY LAYER - PLATES TURBULENT↗
Pressure Distributions on Thin Conical Body of Elliptic Cross Section at Mach Number 1.89
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Maslen, Stephen H↗
Method for calculation of pressure distributions on thin conical bodies of arbitrary cross section in supersonic stream
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THEORIES - FLOW↗