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Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia : final report by Saric, W. S.
Tempe, Ariz. : [Washington, DC] : [Springfield, Va.] : Dept. of Mechanical and Aerospace Engineering, Arizona State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1988Call Number: Loading…
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Design of high-Reynolds-number flat-plate experiments in the NTF final report by Saric, W. S.
Tempe, Ariz. : Dept. of Mechanical and Aerospace Engineering, Arizona State University, 1988Call Number: Loading…
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Swept-wing receptivity studies using distributed roughness : annual technical report by Saric, W. S.
Tempe, AZ : Hampton, Va. : [Springfield, Va.] : Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University ; National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1998Call Number: Loading…
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A generalized magnetohydrodynamic entrance flow model. by Saric, W. S.
[Albuquerque], [Sandia Corp.] 1966Call Number: Loading…
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5
Effects of suction on swept-wing transition : final technical report on NASA-Langley award # NAG-1-194, 16 December 1995 to 31 March 1998 by Saric, W. S.
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1998Call Number: Loading…
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Design of high-Reynolds-number flat-plate experiments in the NTF : final report by Saric, W. S.
Tempe, Ariz. : Dept. of Mechanical and Aerospace Engineering, Arizona State University, 1988Call Number: Loading…
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7
Effect of sound on boundary layer stability : final report submitted to NASA Ames Research Center, cooperative agreement NCC2-659 by Saric, W. S.
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1993Call Number: Loading…
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Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel : final report by Saric, W. S.
[Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995Call Number: Loading…
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9
Crossflow stability and transition experiments in swept-wing flow by Dagenhart, J. Ray
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999Other Authors: “…Saric, W. S.…”
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10
Distributed-roughness effects on stability and transition in swept-wing boundary layers : annual technical report ... NASA-Langley cooperative agreement # NCC-1-194 and the Boeing... by Carrillo, Ruben B.
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997Other Authors:Call Number: Loading…
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11
Laminar-turbulent transition : IUTAM Symposium, Sedona/AZ, September 13-17, 1999
Berlin ; New York : Springer, 2000Other Authors:Call Number: Loading…
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12
Stability in convective flows : presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Miami Beach, Florida, November 17-22, 1985
New York, N.Y. (345 E. 47th St., New York 10017) : The Society, 1985Other Authors: “…Saric, W. S.…”
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Related Subjects
Swept wings
Boundary layer transition
Cross flow
Wind tunnel tests
Aeronautical laboratories
Aeronautics
Airfoils
Boundary layer
Boundary layer control
Boundary layer stability
Fluid dynamics
Laminar boundary layer
Research
Blowing
Boundary layers
Congresses
Convection
Drag reduction
Experimentation
Flow visualization
Heat
Laminar flow
Magnetohydrodynamics
Nonlinearity
Perforated plates
Pressure gradients
Rayleigh number
Reynolds number suction
Sound
Suction