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Concerning the interaction of non-stationary cross-flow vortices in a three-dimensional boundary lay

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

A coupled probabilistic wake vortex and aircraft response prediction model

Gloudemans, Thijs, author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2016. 2016-

Discrete-vortex model for the symmetric-vortex flow on cones

Gainer, Thomas G.
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

An experimental investigation of the ground vortex created by a moving jet

Stewart, V. R.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

Flight validation of a pulsed smoke flow visualization system

Ward, Donald T.
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service], 1993. 1993

The fully nonlinear development of Gortler vortices in growing boundary layers

Hall, Philip, author.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1987] 1987

Initial circulation and peak vorticity behavior of vortices shed from airfoil vortex generators

Wendt, Bruce J.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001] 2001

Instabilities and subharmonic resonances in subsonic heated round jets

Ng, Lian Lai.
[Tucson, Ariz.] : University of Arizona, Dept. of Aerospace and Mechanical Engineering, 1990. 1990

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

Modeling of vortex-induced oscillations based on indicial response approach

Truong, Khiem Van.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1990] 1990

NACA 0015 wing pressure and trailing vortex measurements

McAlister, Kenneth W.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service , distributor], 1991. 1991

Near-planar TS waves and longitudinal vortices in channel flow nonlinear interaction and focusing

Hall, P.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

A new methodology for free wake analysis using curved vortex elements

Bliss, Donald B.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987. 1987

Pressure measurements of impinging jet with asymmetric nozzle progress report

Ho, Chih-Ming.
Los Angeles, Calif. : Dept. of Aerospace Engineering, University of Southern California ; Hampton, VA : NASA Langley Research Center, [1988] 1988

Semi-annual status report on NASA grant NAG 1-1087 "identification of aerodynamic models for maneuve

Chin, Suei.
Lawrence, Kan. : Flight Research Laboratory, The University of Kansas Center for Research, Inc., [1990] 1990

Shear layer excitation, experiment versus theory

Bechert, Dietrich W.
Cleveland, Ohio : NASA Lewis Research Center ; Gottingen, Germany : Institut fur Experimentelle Stromungsmechanik, [1984] 1984

Study for prediction of rotor/wake/fuselage interference

Clark, D. R.
Redmond, WA : Analytical Methods, Inc. ; Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, [1985] 1985

A study of the temporal stability of multiple cell vortices

Khorrami, Mehdi R.
[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], 1989. 1989

Subsonic flow investigations on a cranked wing designed for high maneuverability

Rao, Dhanvada M.
Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1986] 1986

The thermal-vortex equations final report

Shebalin, John V., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [1987] 1987

A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction

Bockelie, Michael J.
[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

Vortex/boundary-layer interaction semi-annual status report on research grant no. NAGW-581

Bradshaw, P. (Peter), 1935-
London : Imperial College of Science and Technology, Dept. of Aeronautics ; [Washington, D.C. : National Aeronautics and Space Administration, 1987] 1987

Vortex breakdown incipience theoretical considerations

Berger, Stanley A., 1934-2013.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1992] 1992