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Application of laminar flow control to supersonic transport configurations

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Effect of flow oscillations on cavity drag and a technique for their control

Gharib, M.
Pasadena, Calif. : National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology, [1985] 1985

An exploratory investigation of a slotted, natural-laminar-flow airfoil

Somers, Dan M.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012] 2012

Flexible micropost arrays for shear stress measurement

Wohl, Christopher J., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2015. 2015-

Large-eddy/Lattice Boltzmann simulations of micro-blowing strategies for subsonic and supersonic dra

Menon, Suresh.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2003] 2003

A novel potential viscous flow coupling technique for computing helicopter flow fields

Summa, J. Michael.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1990] 1990

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20

Capone, Francis J.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992. 1992

Robust airfoil optimization to achieve consistent drag reduction over a mach range

Li, Wu.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2001] 2001