7 resultados para PRESSURE EFFECTS
em University of Michigan
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Transportation Systems Center, Cambridge, Mass.
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"It is shown that adequate means are available for calculating inviscid direct and induced pressures on simple axisymmetric bodies at zero angle of attack. The extent to which viscous effects can alter these predictions is indicated. It is also shown that inviscid induced pressures can significantly affect the stability of blunt, two-dimensional flat wings at low angles of attack. However, at high angles of attack, the inviscid induced pressure effects are negligible."
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Transportation Department, Office of Noise Abatement, Washington, D.C.
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Mode of access: Internet.
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Cover title.
Resumo:
"Materials Central, Contract no. 33(616)-5995. Project no. 7351.
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"Carried out by the Fluid Mechanics Section of the Aeronutronic Division of the Ford Aerospace & Communications Corporation."