Research Catalog
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Displaying 1-6 of 6 results
The use of cowl camber and taper to reduce rotor/stator interaction noise [microform] / R. Martinez.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Final report, Space Station Furnace Facility Management Information System (SSFF-MIS) development [microform] / prepared by Camber Corporation.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65̊ delta wings varying in leading-edge radius and camber [microform] / S. Naomi McMillin ... [et al.].
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
The construction of airfoil pressure models by the bonded plate method [microform] : achievements, current research, technology development and potential applications / Pierce L. Lawing.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
- 1985
Numerical analysis of a variable camber rotor blade as a lift cotrol device [microform] / Alfred O. Awani [and] Robert H. Stroub.
- Text
- Lawrence, Kans : Flight Research Laboratory, University of Kansas Center for Research, Inc. ; [Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, 1984]
- 1984
Delta wings with shock-free cross flow [microform] / S.S. Sritharan.
- Text
- Hampton, Va. : institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
- 1984
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