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Adaptive grid embedding for the two-dimensional flux-split Euler equations

Warren, Gary Patrick.
Mississippi State, Miss. : Mississippi State University, Dept. of Aerospace Engineering, [1990] 1990

Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomach

Athavale, M. M.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2005] 2005

An approximate method for calculating three-dimensional inviscid hypersonic flow fields

Riley, Christopher J. (Christopher Joseph), 1964-
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

Autoclave processing for composite material fabrication. 1. An analysis of resin flows and fiber com

Hou, T. H.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests)

Arrington, E. Allen.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2011

A CFD study of tilt rotor flowfields

Fejtek, Ian.
Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, [1989] 1989

Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Del

Craig, Ken.
Stanford, Calif. : Stanford University, Dept. of Aeronautics and Astronautics ; [Moffett Field, Calif.?] : National Aeronautics and Space Administration, Ames Research Center, 1991] 1991

Contraction design for small low-speed wind tunnels

Bell, J. H.
[Moffett Field, Calif.?] : National Aeronautics and Space Administration, Ames Research Center ; Stanford, CA : Stanford University, Joint Institute for Aeronautics and Acoustics, [1988] 1988

A data base and analysis program for shuttle main engine dynamic pressure measurements final report

Coffin, Thomas.
[Huntsville, Ala.] : Wyle Laboratories Scientific Services & Systems Group ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986] 1986

Design and calibration of the mixing layer and wind tunnel

Bell, James H.
[Stanford, CA] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, Stanford University, [1989] 1989

Development of an actuator for flow control utilizing detonation

Lonneman, Patrick J.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2004] 2004

Development of detonation modeling capabilities for rocket test facilities: hydrogen-oxygen-nitrogen

Allgood, Daniel C., author.
Stennis Space Center, MS : National Aeronautics and Space Administration, Stennis Space Center, April 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

The effect of wake passing on turbine blade film cooling

Heidmann, James D., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996. 1996-

The effects of forcing on a single stream shear layer and its parent boundary layer

Haw, Richard C.
East Lansing, MI : College of Engineering, Michigan State University, [1990] 1990

Effects of inlet flow conditions on crossflow jet mixing

Liscinsky, D. S. (David S.), author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996. 1996-

Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows p

Singh, D. J.
Norfolk, Va. : Old Dominion University Research Foundation ; [Springfield, Va. : National Technical Information Service, distributor, 1990] 1990

Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speed

Plentovich, Elizabeth B.
[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], 1991. 1991

Enhanced design of turbo-jet LPT by separation control using phased plasma actuators

Corke, Thomas C.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Administration ; Springfield, VA : National Technical Information Service [distributor, 2003] 2003

Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment

Miles, Richard B. (Richard Bryant), 1948-
Princeton, N.J. : Princeton University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983] 1983

Experimental investigation of crater growth dynamics semiannual report

Seattle, Wash. : Boeing Aerospace Company ; [Washington, D.C.] : National Aeronautics and Space Administration, [1985] 1985

Experimental visualization of flows in packed beds of spheres

Hendricks, Robert C., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1997. 1997-

Extension of a three-dimensional viscous wing flow analysis

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

Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass tr

Bhat, M. K.
Tullahoma, TN : The University of Tennessee Space Institute ; [Moffett Field, CA] : NASA Ames Research Center ; [Springfield, VA :: For sale by the National Technical Information Service, 1990] 1990

Flowfield computation of entry vehicles

Prabhu, Dinesh K.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990] 1990

High speed turboprop aeroacoustic study (counterrotation)

Whitfield, C. E.
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va.? : National Technical Information Service, distributor, 1990] 1990

Inlet flow control and prediction technologies for embedded propulsion systems summary report for fi

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

Investigation of advanced counterrotation blade configuration concepts for high speed turboprop syst

Hall, Edward J.
[Washington, D.C.] : National Aeronautics and Space Administration, [1990] 1990

Jet noise physics and modeling using first-principles simulations

Freund, Jonathan B.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003] 2003

Jet vortex generators for turbulent flow separation control

Selby, Gregory V. (Gregory Vincent)
Norfolk, Va. : Old Dominion University Research Foundation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990] 1990

Local and global bifurcations of flow fields during physical vapor transport: application to a micro

Duval, Walter M. B., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996. 1996-

Magnetohydrodynamic and gasdynamic theories for planetary bow waves

Spreiter, John R.
[Washington, D.C. : National Aeronautics and Space Administration, 1983?] 1983

Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet

Maglieri, Domenic J.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Measurements and simulations of surface dielectric barrier discharges used as plasma actuators, fina

Hoskinson, Alan R., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

Measurements of a turbulent horseshoe vortex formed around a cylinder

Eckerle, Wayne Alan.
East Hartford, CT : United Technologies Research Center ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1986] 1986

A multi-domain spectral method for supersonic reactive flows

Don, Wai-Sun.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002] 2002

Near-wall modelling of compressible turbulent flows a semi-annual progress report

So, Ronald M. C.
Tempe, Ariz. : Arizona State University ; Hampton, VA : NASA Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990] 1990

Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields semiannual progress

Carlson, Leland A.
College Station, TX : Aerospace Engineering Dept., Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1990] 1990

Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields semiannual progress

Carlson, Leland A.
College Station, TX : Aerospace Engineering Dept., Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1991

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

Numerical flow visualization in basic- and hyper-cluster spheres

Hendricks, Robert C., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, February 1997. 1997-

Numerical simulation of particle-wave interaction in boudary layers final report for NAG-1-798

Biringen, Sedat.
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991] 1991

On computations of the integrated space shuttle flowfield using overset grids final report

Chiu, I.-T.
[Ames, Iowa] : Iowa State University, Engineering Research Institute ; [Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1990] 1990

On the receptivity and non-parallel stability of traveling disturbances in rotating disk flow

Balakumar, P.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering ; [Springfield, Va. : For sale by the National Technical Information Service, 1990] 1990

Optical and probe determination of soot concentrations in a model gas turbine combustor

Eckerle, Wayne Alan.
East Hartford, CT : United Technologies Research Center : Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1986] 1986

Optimum shape of a blunt forebody in hypersonic flow

Maestrello, L.
Hampton, Va. : NASA Langley Research Center, [1989] 1989

A package for 3-D unstructured grid generation, finite-element flow solution and flow field visualiz

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

Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating flow wind tunnel progr

Cook, William John, 1929-
Ames, Iowa : Engineering Research Institute, Iowa State University, [1984] 1984

Phase averaged measurements of the coherent structure of a Mach number 0.6 jet

Emami, Saied, author.
[College Station, TX] : Texas A&M University ; [Washington D.C. : National Aeronautics and Space Administration], December 1983. 1983-

Predicting modes of the unsteady vorticity field near the trailing edge of a blade

Devenport, William J.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003] 2003