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Crossflow stability and transition experiments in swept-wing flow [microform] / J. Ray Dagenhart, William S. Saric.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Method of measuring cross-flow vortices by use of an array of hot-film sensors [microform] / inventors, Naval K. Agarwal, Dal V. Maddalon.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
A computational examination of directional stability for smooth and chined forebodies at High-α [microform] / Ramakrishnan Ravi and William H. Mason.
Microform
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
1992
0 resources
Quick-mixing studies under reacting conditions [microform] : under grant NAG3-1110 / May Y. Leong and G.S. Samuelsen.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
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.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
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).
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Physical mechanisms of glaze ice scallop formations on swept wings [microform] / Mario Vargas, Eli Reshotko.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Optimization of jet mixing into a rich, reacting crossflow [microform] / M.Y. Leong and G.S. Samuelsen, J.D. Holdeman.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : Available from National Technical Information Service, distributor, [1998]
1998
0 resources
The effect of vortex generators on a jet in a cross-flow [microform] / K.B.M.Q. Zaman and J.K. Foss.
Microform
[Woodbury, NY] : American Institute of Physics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor], 1997.
1997
0 resources
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.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
The effects of crossflow on the pressures and lift induced by the fountain generated between two impinging jets [microform] / Richard E. Kuhn.
Microform
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Dynamics of large-scale structures for jets in crossflow [microform] / Frank Muldoon and Sumanta Acharya.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Swept-wing receptivity studies using distributed roughness [microform] : annual technical report / William S. Saric.
Microform
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
0 resources
Pegasus wing-glove experiment to document hypersonic crossflow transition [microform] : measurement system and selected flight results / Arild Bertelrud ... [et al.].
Microform
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
0 resources
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.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
2000
0 resources
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].
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2000]
2000
0 resources
Natural laminar flow flight experiments on a swept wing business jet [microform] : boundary layer stability analyses / R. A. Rozendaal.
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
Concerning the interaction of non-stationary cross-flow vortices in a three-dimensional boundary layer [microform] / Andrew P. Bassom, Philip Hall.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
Delta wings with shock-free cross flow [microform] / S.S. Sritharan.
Microform
Hampton, Va. : institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
1984
0 resources
Heat transfer distributions around nominal ice accretion shapes formed on a cylinder in the NASA Lewis icing research tunnel [microform] / G. J. Van Fossen, ... [et al.].
Microform
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
1 resource
Available online
Flow visualization study of the effect of injection hole geometry on an inclined jet in crossflow [microform] / Frederick F. Simon and Michael L. Ciancone.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, [1985]
1985
0 resources
Effects of velocity profile and inclination on dual-jet-induced pressures on a flat plate in a crosswind [microfiche] / A. K. Jakubowski ... [et al.].
Microform
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
1985
0 resources
A critical evaluation of various methods for the analysis of flow-solid interaction in a nest of thin cylinders subjected to cross flows [microform] : interim report / by Sang-Wook Kim.
Microform
Marshall Space Flight Center, Ala. : NASA-Marshall Space Flight Center, Systems Dynamics Laboratory, Science and Engineering Directorate, [1987]
1987
0 resources
Measurements of a single lateral jet injected into swirling crossflow / L.H. Ong and D.G. Lilley.
Microform
Washington, D.C. : National Aeronautics and Space Administration, January 1986.
1986
0 resources