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Photon correlation techniques in fluid mechanics : proceedings ... / edited by W. T. Mayo, Jr. and A. E. Smart ; [organized by the Joint Institute for Aeronautics and Acoustics, Stanford University and Spectron Development Laboratories ; under the sponsorship of the Office of Naval Research ... et al.].

Text

[S.l. : s.n.], 1980.

1980

1 item

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Forebody tangential blowing for control at high angles of attack [microform] : feasibility study final report / by I. Kroo and L. Roberts.

Text

Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics ; [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center, [1991]

1991

0 resources

A numerical study of the effects of wind tunnel wall proximity on an airfoil model [microform] / by Mark Potsdam and Leonard Roberts.

Text

Stanford, Calif. : Stanford University, Dept. of Aeronautics and Astronautics ; [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center, [1990]

1990

0 resources

Analysis of a dusty wall jet [microform] / by Hock-Bin Lim and Leonard Roberts.

Text

Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics ; [Springfield, Va. : National Technical Information Service, distributor, 1991]

1991

0 resources

An experimental study of an adaptive-wall wind tunnel [microform] / by Zeki Celik and Leonard Roberts.

Text

Stanford, CA : Joint Institute for Aeronautics and Acoustics, Stanford University, Dept. of Aeronautics and Astronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]

1988

0 resources

A zonal computational procedure adapted to the optimization of two-dimensioal thrust augmentor inlets [microform] / by T.S. Lund, D.A. Tavella, and L. Roberts.

Text

Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : National Aeronautics and Space Administration, Ames Research Center, Joint Institute for Aeronautics and Acoustics ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]

1985

0 resources

Flow past a flat plate with a vortex/sink combination [microform] / Nikos J. Mourtos ; Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center ; Stanford University.

Text

Stanford, Calif. : Stanford University, Dept. of Aeronautics and Astronautics ; [Moffett Field, Calif. : The Center : Springfield, Va. : National Technical Information Service, distributor, 1984]

1984

0 resources

A study of the factors affecting boundary layer two-dimensionality in wind tunnels [microform] / by R.D. Mehta and P.H. Hoffmann.

Text

Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : Joint Institute for Aeronautics and Acoustics ; [Springfield, Va. : National Technical Information Service, distributor, 1986]

1986

0 resources

An analysis of blade vortex interaction aerodynamics and acoustics [microform] / by Duck Joo Lee.

Text

Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : Joint Institute for Aeronautics and Acoustics ; [Springfield, Va. : National Technical Information Service, distributor, 1985]

1985

0 resources

Analytical observations on the aerodynamics of a delta wing with leading edge flaps [microform] / by Sejong Oh and Domingo Tavella.

Text

Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : Joint Institute for Aeronautics and Acoustics ; [Springfield, Va. : National Technical Information Service, distributor, 1986]

1986

0 resources

The art of sharp-leading-edged delta wings with blowing [microform] / Domingo A. Tavella.

Text

Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : Joint Institute for Aeronautics and Acoustics ; [Springfield, Va. : National Technical Information Service, distributor, 1985]

1985

0 resources

Direct numerical simulation of a temporally evolving incompressible plane wake [microform] : effect of initial conditions on evolution and topology / R. Sondergaard, B. Cantwell, and N. Mansour.

Text

Stanford, CA : Joint Institute for Aeronautics and Acoustics ; [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

0 resources

Roll-yaw control at high angle of attack by forebody tangential blowing [microform] / N. Pedreiro ... [et al.].

Text

[Stanford, Calif.?] : Joint Institute for Aeronautics and Acoustics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]

1995

0 resources

Application of the pressure sensitive paint technique to steady and unsteady flow [microform] / Y. Shimbo, R. Mehta, B. Cantwell.

Text

[Stanford, Calif.?] : Joint Institute for Aeronautics and Acoustics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]

1996

0 resources

Experimental study of vortex breakdown in a cylindrical, swirling flow [microform] / J.L. Stevens ... [et al.].

Text

[Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]

1996

0 resources

Development of an apparatus for wind tunnel dynamic experiments at high-α [microform] / Nelson Pedreiro.

Text

[Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

0 resources

Self-similar compressible free vortices [microform] / Karl von Ellenrieder.

Text

[Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1998]

1998

0 resources

Experiments in aircraft roll-yaw control using forebody tangential blowing [microform] / Nelson Pedreiro.

Text

[Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

0 resources

Transpiration cooling in hypersonic flight [microform] / Domingo Tavelia and Leonard Roberts.

Text

Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]

1989

1 resource

Available online

http://purl.access.gpo.gov/GPO/LPS62036

A CFD study of tilt rotor flowfields [microform] / by Ian Fejtek and Leonard Roberts.

Text

Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, [1989]

1989

1 resource

Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings [microform] / by Ken Craig.

Text

Stanford, Calif. : Stanford University, Dept. of Aeronautics and Astronautics ; [Moffett Field, Calif.?] : National Aeronautics and Space Administration, Ames Research Center, 1991]

1991

1 resource

Contraction design for small low-speed wind tunnels / by James H. Bell and Rabindra D. Mehta.

Text

[Moffett Field, Calif.?] : National Aeronautics and Space Administration, Ames Research Center ; Stanford, CA : Stanford University, Joint Institute for Aeronautics and Acoustics, [1988]

1988

1 resource

Contraction design for small low-speed wind tunnels [microform] / by James H. Bell and Rabindra D. Mehta.

Text

[Moffett Field, Calif.?] : National Aeronautics and Space Administration, Ames Research Center ; Stanford, CA : Stanford University, Joint Institute for Aeronautics and Acoustics, [1988]

1988

1 resource

An experimental study of airfoil-spoiler aerodynamics [microform] / Blair G. McLachlan and K. Karamcheti.

Text

Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]

1985

0 resources

Design and calibration of the mixing layer and wind tunnel / by James H. Bell and Rabindra D. Mehta.

Text

[Stanford, CA] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, Stanford University, [1989]

1989

1 resource

Design and calibration of the mixing layer and wind tunnel [microform] / by James H. Bell and Rabindra D. Mehta.

Text

[Stanford, CA] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, Stanford University, [1989]

1989

0 resources

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