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  • Crossflow stability and transition experiments in swept-wing flow [microform] / J. Ray Dagenhart, William S. Saric.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Characteristics of 3D turbulent jets in crossflow [microform] / A.O. Demuren.

    • Text
    • [Cleveland, Ohio] : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • The effects of vortex ingestion on the flow in a diffusing S-DUCT [microform] / B.J. Wendt and B.A. Reichert.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Modeling jets in cross flow [microform] / A.O. Demuren.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application [microform] / Kamlesh Kapoor, Bernard H. Anderson, and Robert J. Shaw.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters [microform] / Cynthia A. Crowell and Henry L. Kelley.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • A laser Doppler velocimeter approach for near-wall three-dimensional turbulence measurements [microform] / D.A. Johnson and J.D. Brown.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Vortex instabilities in 3D boundary layers [microform] : the relationship between Görtler and crossflow vortices / Andrew P. Bassom nad Philip Hall.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • 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

  • Nonlinear instability of a uni-directional transversely sheared mean flow [microform] / David W. Wundrow and Marvin E. Goldstein.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Effect of crossflow on Görtler instability in incompressible boundary layers [microform] / Y.H. Zurigat, M.R. Malik.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Method of measuring cross-flow vortices by use of an array of hot-film sensors [microform] / inventors, Naval K. Agarwal, Dal V. Maddalon.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Experimental results of the control of a vortical flow by tangential blowing [microform] / N.J. wood and L. Roberts.

    • Text
    • Stanford, Calif. : Stanford University, Dept. of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • The influence of jet-grid turbulence on heat transfer from the stagnation region of a cylinder in crossflow [microform] / James E. O'Brien and G. James VanFossen, Jr.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Flow in out-of-plane double s-bends [microform] / by M.C. Schmidt, J.H. Whitelaw and M. Yianneskis.

    • Text
    • London, England : Imperial College of Science and Technology, Fluids Section, Mechanical Enginering Dept. : [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Measurements of wing-tip blowing [microform] / by D. Tavella, N. Wood and P. Harrits.

    • Text
    • [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Turbine blade and vane heat flux sensor development phase 2 [microform] / by W.H. Atkinson, M.A. Cyr, R.R. Strange.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, distributor, [1985]
    • 1985

  • Jet mixing and emission characteristics of transverse jets in annular and cylindrical confined crossflow [microform] / D.B. Bain and C.E. Smith, J.D. Holdleman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Effects of initial conditions on a single jet in crossflow [microform] / D.S. Liscinsky and B. True, J.D. Holdeman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • The decay of longitudinal vortices shed from airfoil vortex generators [microform] / Bruce J. Wendt, Bruce A. Reichert, Jeffry D. Foster.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Crossflow mixing of noncircular jets [microform] / D.S. Liscinsky and B. True, J.D. Holdeman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Jet mixing in a reacting cylindrical crossflow [microform] / M.Y. Leong and G.S. Samuelsen, J.D. Holdeman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Effect of density gradients in confined supersonic shear layers [microform] / Oshin Peroomian and R.E. Kelly.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Weakly nonparallel and curvature effects on stationary crossflow instability [microform] : comparison of results from multiple-scales analysis and parabolized stability equations / Bart A. Singer, Meelan Choudhari, and Fei Li.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • The effect of crossflow on Görtler vortices [microform] / S.R. Otto, James P. Denier.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • On the nonlinear evolution of a stationary cross-flow vortex in a fully three-dimensional boundary layer flow [microform] / J.S.B. Gajjar.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Calculation of 3D turbulent jets in crossflow with a multigrid method and a second-moment closure model [microform] / A.O. Demuren ; prepared for the International Symposium on Engineering Turbulence Modelling and Measurements, sponsored by the Assembly of World Conferences on Experimental Heat Transfer, Fluid Mechanics, and Thermodynamics, Dubrovnik, Yugoslavia, September 24-28, 1990.

    • Text
    • Cleveland,Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : For sale by the National Technical Information Service, 1990?]
    • 1990

  • Simulation of crossflow instability on a supersonic highly swept wing [microform] / C. David Pruett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Effects of inlet conditions on crossflow jet mixing [microform] / D.S. Liscinsky and B. True, J.D. Holderman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Mixing of pure air jets with a reacting fuel-rich crossflow [microform] / M.Y. Leong and G.S. Samuelsen, J.D. Holdeman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Mixing of multiple jets with a confined subsonic crossflow [microform]. Part II, opposed rows of orifices in rectangular ducts / James D. Holdeman, David S. Liscinsky, Daniel B. Bain.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Three dimensional viscous flow field in an axial flow turbine nozzle passage [microform] / D. Ristiʹc and B. Lakshminarayana.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • A new approach for determining onset of transition [microform] : final report : NASA grant NAG-1-1876 / prepared by H.A. Hassan.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Study of injection of helium into supersonic air flow using Rayleigh scattering [microform] / Richard G. Seasholtz and Alvin E. Buggele.

    • Text
    • 1997

  • A computational examination of directional stability for smooth and chined forebodies at High-α [microform] / Ramakrishnan Ravi and William H. Mason.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
    • 1992

  • Quick-mixing studies under reacting conditions [microform] : under grant NAG3-1110 / May Y. Leong and G.S. Samuelsen.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Effects of suction on swept-wing transition [microform] : final technical report on NASA-Langley award # NAG-1-194, 16 December 1995 to 31 March 1998 / by William S. Saric.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Distributed-roughness effects on stability and transition in swept-wing boundary layers [microform] : annual technical report ... NASA-Langley cooperative agreement # NCC-1-194 and the Boeing Company contract #ZA0078, during 5/17/96-12/31/96 / submitted by Ruben B. Carrillo, Jr.; Mark S. Reibert; William S. Saric (principal investigator).

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Physical mechanisms of glaze ice scallop formations on swept wings [microform] / Mario Vargas, Eli Reshotko.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Optimization of jet mixing into a rich, reacting crossflow [microform] / M.Y. Leong and G.S. Samuelsen, J.D. Holdeman.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : Available from National Technical Information Service, distributor, [1998]
    • 1998

  • The effect of vortex generators on a jet in a cross-flow [microform] / K.B.M.Q. Zaman and J.K. Foss.

    • Text
    • [Woodbury, NY] : American Institute of Physics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Atomization and dispersion of a liquid jet injected into a crossflow of air [microform] : under grant NAG3-1124 / J.E. Seay and G.S. Samuelsen.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • The effects of crossflow on the pressures and lift induced by the fountain generated between two impinging jets [microform] / Richard E. Kuhn.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Dynamics of large-scale structures for jets in crossflow [microform] / Frank Muldoon and Sumanta Acharya.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Swept-wing receptivity studies using distributed roughness [microform] : annual technical report / William S. Saric.

    • Text
    • Tempe, AZ : Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Pegasus wing-glove experiment to document hypersonic crossflow transition [microform] : measurement system and selected flight results / Arild Bertelrud ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, Va. : National Technical Information Service [distributor, 2000]
    • 2000

  • Effect of jet injection angle and number of jets on mixing and emissions from a reacting crossflow at atmospheric pressure [microform] / D. St. John and G. S. Samuelsen.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • Mixing of an airblast-atomized fuel spray injected into a crossflow of air [microform] / May Y. Leong, Vincent G. McDonell, and G. Scott Samuelsen ; [prepared under cooperative agreement NCC3-412].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2000]
    • 2000

  • Natural laminar flow flight experiments on a swept wing business jet [microform] : boundary layer stability analyses / R. A. Rozendaal.

    • Text
    • [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

  • Concerning the interaction of non-stationary cross-flow vortices in a three-dimensional boundary layer [microform] / Andrew P. Bassom, Philip Hall.

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

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