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Rapid numerical simulation of viscous axisymmetric flow fields / Daniel L. Tweedt and Rodrick V. Chima.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va.] : [National Technical Information Service, distributor], [1995]
1995
0 resources
Blockage development in a transonic, axial compressor rotor [microform] / Kenneth L. Suder.
Microform
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] / John W. Edwards.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
An efficient multiblock method for aerodynamic analysis and design on distributed memory systems [microform] : to be presented at the AIAA 13th Computational Fluid Dynamics Conference, June 1997 / James Reuther ... [et al.].
Microform
[Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Optimum transonic airfoils based on the Euler equations [microform] / Angelo Iollo, Manuel D. Salas.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Navier-Stokes computations on full wing-body configuration with oscillating control surfaces [microform] / Shigeru Obayashi, Ing-Tsau Chiu, Guru P. Guruswamy.
Microform
Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Natural rolling responses of a delta wing in transonic and subsonic flows [microform] / Margaret A. Menzies and O. Kandil.
Microform
Reston, Va. : American Institute of Aeronautics and Aeronautics ; [Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Unsteady, transonic flow around delta wings undergoing coupled and natural modes response : a multidisciplinary problem / by Margaret Anne Menzies ; a dissertation submitted to the Faculty of Old Dominion University in partial fulfillment of the requirement for the degree of Doctor of Philosophy, Aerospace Engineering, Old Dominion University.
Microform
[Norfolk, VA : Old Dominion University ; Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Final report for NASA Ames cooperative agreement, NCC2-5049 [microform].
Microform
[Davis, Calif.] : Dept. of Mechanical and Aeronautical Engineering, University of California ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
A numerical simulator for three-dimensional flows through vibrating blade rows [microform] / H. Andrew Chuang and Joseph M. Verdon.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Globalized Newton-Krylov-Schwarz algorithms and software for parallel implicit CFD [microform] / W.D. Gropp ... [et al.].
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Experimental investigation of the flow field in a transonic, axial flow compressor, with respect to the development of blockage and loss / Kenneth L. Suder.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Three-dimensional flow field measurements in a transonic turbine [microform] / P.W. Giel ... [et al.].
Microform
[Washington, DC] : National Aeronautics and Space Administration : U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Current Lewis turbomachinery research [microform] : building on our legacy of excellence / Louis A. Povinelli.
Microform
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] : EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996 / John W. Edwards.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Full-potential modeling of blade-vortex interactions [microform] / Henry E. Jones.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Assessment of two-equation turbulence models for transonic flows [microform] / Florian R. Menter, Christopher L. Rumsey.
Microform
Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data [microform] / Daryl L. Bonhaus and Dal V. Maddalon.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
MAVRIC flutter model transonic limit cycle oscillation test [microform] / John W. Edwards ... [et al.].
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
2001
1 resource
Available online
Calibration of sonic valves for the laminar flow control, leading-edge flight test [microform] / Dennis H. Petley ... [et al.].
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service,] 1985.
1985
0 resources
Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment [microform] / James T. Howlett and Samuel R. Bland.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
1987
0 resources
Flow prediction for propfan engine installation effects on transport aircraft at transonic speeds [microform] / S. S. Samant and N. J. Yu.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
1986
0 resources
Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds [microform] / Charles W. Boppe.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
1987
1 resource
Available online
An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients [microform] : semiannual progress report, January 1991 - June 1991 / Leland A. Carlson.
Microform
College Station, Tex. : Aerospace Engineering Dept., Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration, 1991]
1991
1 resource
Available online
Euler flow predictions for an oscillating cascade using a high resolution wave-split scheme [microform] / Dennis L. Huff, Timothy W. Swafford, and T.S.R. Reddy.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
1991
1 resource
Available online
Calculations of steady and transient channel flows with a time-accurate L-U factorization scheme [microform] / S.-W. Kim.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by National Technical Information Service, 1991]
1991
1 resource
Available online
An incremental strategy for calculating consistent discrete CFD sensitivity derivatives [microform] / Vamshi Mohan Korivi ... [et al.].
Microform
Hampton, VA : National Aeronautics and Space Administration, Langley Research Center ; [St. Louis, MO] : US Army Aviation Systems Command, [1992]
1992
1 resource
Available online
Extension of transonic flow computational concepts in the analysis of cavitated bearings [microform] / D. Vijayaraghavan, T.G. Keith, Jr., and D.E. Brewe.
Microform
[Cleveland, Ohio : Lewis Research Center, 1990]
1990
1 resource
Available online
Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer [microform] / by M.K. Bhat, A.D. Vakili, and J.M. Wu.
Microform
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
1 resource
Available online
Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. Task 1, Ducted propfan analysis [microform] : final report / Edward J. Hall, Robert A. Delaney, and James L. Bettner.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, [1990]
1990
1 resource
Available online
Validation of viscous and inviscid computational methods for turbomachinery components [microform] / Louis A. Povinelli.
Microform
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
1986
0 resources
Unsteady transonic flow calculations for wing-fuselage configurations [microform] / John T. Batina.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
1986
0 resources
The construction of airfoil pressure models by the bonded plate method [microform] : achievements, current research, technology development and potential applications / Pierce L. Lawing.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Inlet flowfield investigation. Part I. Transonic flowfield survey [microform].
Microform
Seattle, Wash. : Boeing Military Airplane Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
1983
0 resources
Newton like [microform] : minimal residual methods applied to transonic flow calculations / Yau Shu Wong.
Microform
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
1984
0 resources
Results of the integration of a transonic full-potential analysis program with a free-wake lifting-line program for hovering rotors [microform] / Song-Young Chung.
Microform
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1987]
1987
1 resource
Available online
Entropy condtion satisfying approximations for the full potential equations of transonic flow [microform] / Stanley Osher, Woodrow Whitlow, Jr., and Mohamed Hafez.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
1984
0 resources
XTRAN2L [microform] : a program for solving the general-frequency unsteady transonic small disturbance equation / Woodrow Whitlow, Jr.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
1983
0 resources
Unsteady transonic flow calculations for two-dimensional canard-wing configurations with aeroelastic applications [microform] / John T. Batina.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads [microform] / John T. Batina.
Microform
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
1985
1 resource
Available online
Viscous effects on transonic airfoil stability and response [microform] / H. M. Berry, J. T. Batina, T. Y. Yang.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Comparison of calculated and measured pressures on straight-and swept-tip model rotor blades [microform] / Michael E. Tauber, ... [et al.].
Microform
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
1983
0 resources
Reduction of the shock wave intensity by modifying the transsonic [i.e. transonic] blade trailing edge [microform] / Piotr Doerffer.
Microform
Washington, D.C. : National Aeronautics and Space Administration, [1983]
1983
0 resources
Efficient self-consistent viscous-inviscid solutions for unsteady transonic flow [microform] / James T. Howlett.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Measured unsteady transonic aerodynamic characteristics of an elastic supercritical wing with an oscillating control device [microform] / David A. Seidel, Maynard C. Sanford and Clinton V. Eckstrom.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Numerical calculation of the transonic potential flow past a cranked wing [microform] / I-Chung Chang and Michael Tauber.
Microform
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
1983
0 resources
Calculation of transonic flow in a linear cascade [microform] / Leo F. Donovan.
Microform
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
0 resources
Redesign and cascade tests of a supercritical controlled diffusion stator blade-section [microform] / James F. Schmidt, Thomas F. Gelder, and Leo F. Donovan.
Microform
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
0 resources
Investigation of flow phenomena in a transonic fan rotor using laser anemometry [microform] / Anthony J. Strazisar.
Microform
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
0 resources
Euler solutions using an implicit multigrid technique [microform] / Chien-peng Li.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
1986
0 resources