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Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from mode

Noonan, Kevin W., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980. 1980-

Aerothermal analysis of a wing-elevon cove with variable leakage

Hunt, L. Roane (Lewis Roane), author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980. 1980-

The effects of anisotropic free-stream turbulence on turbulent boundary layer behavior

Fang, Liang-Wei.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985] 1985

The effects of Reynolds number, rotor incidence angle, and surface roughness on the heat transfer di

Blair, Michael F.
East Hartford, Conn. : United Technologies Research Center ; [Washington, D.C. : National Aeronautics and Space Administration, 1989] 1989

Experimental measurements of sonic boom signatures using a continuous data acquistion technique

Wilcox, Floyd J., Jr, author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013. 2013-

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Met

Lawing, Pierce L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980. 1980-

In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0

Quinn, Robert D., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November1980. 1980-

Magnetic flux compression experiments using plasma armatures

Turner, M. W., author.
MSFC, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, March 2003. 2003-

Mean velocity and turbulence measurements in a 90 curved duct with thin inlet boundary layer final r

Tullahoma, Tenn. : University of Tennessee Space Institute ; [Cleveland, Ohio] : NASA Lewis Research Center, [1985] 1985

Wave phenomena in a high Reynolds number compressible boundary layer

Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1985] 1985

Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hol

Stallings, Robert L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-