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Alternate Subjects (1-2 of 2)
Flow Geometry
1
BladeCAD: an interactive geometric design tool for turbomachinery blades
Miller, Perry L., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996. 1996-
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Axe Federal Documents Online
NAS 1.15:107262
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2
ElectronicResource GovDoc
Effects of forebody geometry on subsonic boundary-layer stability
Dodbele, S. S.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990. 1990
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Axe Federal Documents Online
NAS 1.26:4314
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