Active filters
Displaying 1-50 of 107 results
An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique [microform] / Danny P. Hwang.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : Available from National Technical Information Service, [1999]
1999
0 resources
F-16XL-2 supersonic laminar flow control flight test experiment [microform] / Scott G. Anders and Michael C. Fischer.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
1999
0 resources
Final report for NASA grant NAGW-1514, titled, magnetic field waves at Uranus, to the Bartol Research Institute of the University of Delaware, administered under the auspices of the Uranus Data Analysis Program [microform] / Charles W. Smith, principal investigator ... [et al.].
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
An analysis of supersonic flows with low-Reynolds number compressible two-equation turbulence models using LU finite volume implicit numerical techniques [microform] / J. Lee.
Text
[Washington, DC] : National Aeronautics and Space Administration, [1994]
1994
0 resources
Analysis and design of numerical schemes for gas dynamics 1 [microform] : artificial diffusion, upwind biasing, limiters and their effect on accuracy and multigrid convergence / Antony Jameson.
Text
[Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Surface documentation of a 3-D supersonic, shock-wave-boundary layer interaction [microform] / Jeffrey K. Wideman ... [et al.].
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Shear flow control of cold and heated rectangular jets by mechanical tabs [microform] / W.H. Brown and K.K. Ahuja.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
1989
0 resources
Development of a laser-induced heat flux technique for measurement of convective heat transfer coefficients in a supersonic flowfield [microform] / A. Robert Porro ... [et al.].
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1991]
1991
0 resources
Wind tunnel pressure study and Euler code validation of a missile configuration with 77̊ swept delta wings at supersonic speeds [microform] / Patsy S. Fulton.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
A preliminary design study of supersonic through-flow fan inlets [microform] / Paul J. Barnhart.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Comparison of 3D computation and experiment for non-axisymmetric nozzles [microform] / H. Lai and E. Nelson.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
1989
0 resources
The inviscid axisymmetric stability of the supersonic flow along a circular cylinder [microform] / Peter W. Duck.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
1989
0 resources
In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows [microform] : design and development / Kon-Sheng Charles Wang.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
1994
0 resources
Embedded function methods for compressible high speed turbulent flow [microform] : final report / J. D. A. Walker.
Text
Hampton, Va. : NASA Langley Research Center, [1994]
1994
0 resources
Investigation of ramp injectors for supersonic mixing enhancement [microform] / Y. Haimovitch, E. Gartenberg, and A.S. Roberts.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : National Technical Information Service, distributor, 1994]
1994
0 resources
An assessment of the adaptive unstructured tetrahedral grid, Euler flow solver code FELISA [microform] / M. Jahed Djomehri, Larry L. Erickson.
Text
Moffett Field, Calif. : Ames Research Center, National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
1994
0 resources
Potential flow downstream of the heliospheric terminal schock [microform] : a non-spherical schock / Steven Nerney and Steven T. Suess.
Text
Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Instantaneous 2D velocity and temperatire measurements in high speed flows based on spectrally resolved molecular Rayleigh scattering [microform] / Richard G. Seasholtz.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer [microform] : long wave limit / Thomas F. Balsa, James Gartside.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Computation of asymmetric supersonic flows around cones at large incidence [microform] : final report / principal investigator, David Degani.
Text
Technion City, Haifa, Israel : Technion Research & Development Foundation ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987?]
1987
0 resources
Supersonic laminar flow control research [microform] : semiannual report #2 / Dr. C.F. Lo, principal investigator.
Text
Moffett Field, Calif. : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Aeroacoustics of supersonic jet flows from contoured and solid-porous conical plug-nozzles [microform] / Darshan S. Dosanjh and Indu S. Das.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
1987
0 resources
Investigation of supersonic chemically reacting and radiating channel flow [microform] / by Mortaza Mani, Surendra N. Tiwari.
Text
Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations [microform] : user's manual / F.T. Johnson ... [et al.].
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
1992
0 resources
TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations [microform] : theory document / F.T. Johnson ... [et al.].
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
1992
0 resources
Development of an upwind, finite-volume code with finite-rate chemistry [microform] / Gregory A. Molvik.
Text
San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Nonlinear potential analysis techniques for supersonic aerodynamic design [microform] / V. Shankar and K.Y. Szema.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
1985
0 resources
Numerical simulation of shock/turbulent boundary layer interaction [microform] : final year report for NASA grant NAG-1-1472 / principal investigator, Sedat Biringen.
Text
Boulder, Colo. : Dept. of Aerospace Engineering Sciences, University of Colorado ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993?]
1993
0 resources
Numerical simulation of stability and stabiity control of high speed compressible rotating couette flow [microform] : final report for NASA grant NAG-1-1103 / principal investigator, Sedat Biringen, research associate, Ferhat F. Hatay.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
An asymptomatic theory of supersonic propeller noise [microform] / Edmane Envia.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
A numerical method for solving the three-dimensional parabolized Navier-Stokes equations [microform] / Domenic D'Ambrosio, Roberto Marsilio.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Numerical calculations of shock-wave/boundary-layer flow interactions [microform] / P.G. Huang and W.W. Liou.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] : final report / Stephen W.D. Wolf.
Text
San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
An edge-based solution-adaptive method applied to the AIRPLANE code [microform] / Rupak Biswas, Scott D. Thomas, Susan E. Cliff.
Text
[Moffett Field, CA] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Experimental investigation of the inlet deflector configuration variation in the flow field at mach 1.9 [microform] : final report / by Kyu C. Hwang, Surrendra N. Tiwari, and Stanley J. Miley.
Text
Norfolk, VA : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Wing-section optimization for supersonic viscous flow [microform] : [abstract] / Cem C. Item and Oktay Baysal.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Wing-section optimization for supersonic viscous flows [microform] : abstract / Cem C. Item.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis [microform] : final report for the period ended August 15, 1995 / by Oktay Baysal.
Text
Norfolk, Va. : Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Optical techniques for shock visualization and detection [microform] / G. Adamovsky and D.K. Johnson.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Numerical simulation of supersonic flow using a new analytical bleed boundary condition [microform] / G.J. Harloff and G.E. Smith.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Flow characteristics in boundary layer bleed slots with plenum [microform] / A. Hamed, J.J. Yeuan and J.D. Jun.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1995]
1995
0 resources
Supersonic wing and wing-body shape optimization using an adjoint formulation [microform] / James Reuther and Antony Jameson.
Text
[Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Supersonic reacting internal flow fields [microform] / J. Philip Drummond.
Text
[Washington, D.C.? : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990?]
1990
0 resources
Supersonic laminar flow control research [microform] : semiannual report #4, July 1995 - December 1995 / Dr. C.F. Lo, principal investigator.
Text
Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Instrumentation development for study of Reynolds analogy in reacting flows [microform] / D.J. DeTurris.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
The Kirchhoff formulas for moving surfaces in aeroacoustics [microform] : the subsonic and supersonic cases / F. Farassat.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Final summary report under NASA cooperative agreement no. NCC10-0010 entitled "Supersonic Gas-Liquid Cleaning System" research project [microform] / principal investigator, Frank Kinney.
Text
Titusville, Fla. : Technological Research and Development Authority, State of Florida ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Parallelization of a parabolized Navier-Stokes solver with a design optimizer [microform] : 34th AIAA Aerospace Sciences Meeting and Exhibit / J.M. Pallis and J.J. Chattot, S.L. Lawrence.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge [microform] : NASA contract no. NAS1-19480 / Peter W. Duck, D. Glenn Lasseigne, M.Y. Hussaini.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
An extended Lagrangian method [microform] / Meng-Sing Liou.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
No results found from Digital Research Books Beta
Digital books for research from multiple sources worldwide - all free to read, download, and keep. No library card required.
Explore Digital Research Books Beta