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Displaying 1-50 of 492 results

Estimated benefits of variable-geometry wing camber control for transport aircraft [microform] / Alexander Bolonkin, Glenn B. Gilyard.

Text

Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]

1999

0 resources

Development, analysis and testing of the High Speed Research Flexible Semispan Model [microform] / David M. Schuster ... [et al.].

Text

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

1999

0 resources

Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel [microform] / Sharon S. Graves.

Text

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

1999

0 resources

Modeling of longitudinal unsteady aerodynamics of a wing-tail combination [microform] / Vladislav Klein.

Text

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

1999

0 resources

First International Symposium on Strain Gauge Balances [microform] / edited by John S. Tripp and Ping Tcheng.

Text

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

1999

0 resources

Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air [microform] / William I. Scallion.

Text

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

1999

0 resources

Unstructured grid Euler method assessment for longitudinal and lateral/directional aerodynamic performance analysis of the HSR technology concept airplane at supersonic cruise speeds [microform] / Farhad Ghaffari.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service, [distributor, 1999]

1999

0 resources

Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle [microform] / William Herkes.

Text

[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 2000-

2000

0 resources

Navier-Stokes simulation of several high-lift reference H configurations [microform] / Wendy B. Lessard.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]

1999

0 resources

Modeling the high speed research cycle 2B longitudinal aerodynamic database using multivariate orthogonal functions [microform] / E.A. Morelli and M.S. Proffitt.

Text

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

1999

0 resources

Turbulence model comparisons for a high-speed aircraft [microform] / Melissa B. Rivers and Richard A. Wahls.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]

1999

0 resources

Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [et al.].

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]

1999

0 resources

1999 NASA High-Speed Research Program Aerodynamic Performance Workshop [microform] : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., and held in Anaheim, California, February 8-12, 1999 / edited by David E. Hahne.

Text

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

1999-present

0 resources

The history of the XV-15 tilt rotor research aircraft [microform] : from concept to flight / Martin D. Maisel, Demo J. Giulianetti, and Daniel C. Dugan.

Text

Washington, D.C. : National Aeronautics and Space Administration, Office of Policy and Plans, NASA History Division : For sale by the U.S. G.P.O., Supt. of Docs., 2000.

2000

0 resources

Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests) [microform] / E. Allen Arrington and Jose C. Gonsalez, Bonnie A. Kee-Bowling.

Text

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

2000

0 resources

Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 [microform] / Mark C. Davis ... [et al.].

Text

Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 2000]

2000

0 resources

Description and evaluation of an interference assessment method for a slotted-wall wind tunnel [microform] / William B. Kemp, Jr.

Text

Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.

1991

0 resources

Cryogenic wind tunnels [microform] : a comprehensive, annotated bibliography / Marie H. Tuttle, Robert A. Kilgore, Deborah L. Moore.

Text

[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.

1991

0 resources

Experimental uncertainty and drag measurements in the National Transonic facility [microform] / Stephen M. Batill.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept [microform] / David J. Wing.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

Experimental studies of shock-wave/wall-jet interaction in hypersonic flow [microform] / Michael S. Holden, Kathleen Rodriguez.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Center, distributor, 1994]

1994

0 resources

An experimental study of the flowfield on a semispan rectangular wing with a simulated glaze ice accretion [microform] / Abdollah Khodadoust.

Text

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

1994

0 resources

Control of low-speed turbulent separated flow over a backward-facing ramp [microform] / by John C. Lin.

Text

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

1994

0 resources

Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds [microform] / Gloria Hernandez ... [et al.].

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

Role of wind tunnels and computer codes in the certification and qualification of rotorcraft for flight in forecast icing [microform] / Robert J. Flemming, Randall K. Britton, Thomas H. Bond.

Text

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

1994

0 resources

F/A-18 forebody vortex control [microform] / Brian R. Kramer ... [et al.].

Text

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

1994-present

0 resources

Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 [microform] / Ira J. Walker, Peter F. Covell And Dana K. Forrest.

Text

[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.

1993

0 resources

Shock-tunnel combustor testing for hypersonic vehicles [microform] / Mark Loomis.

Text

San Jose, Calif. : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

NASA's hypersonic research engine project [microform] : a review / Earl H. Andrews, Ernest A. Mackley.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

Two-dimensional converging-diverging rippled nozzles at transonic speeds [microform] / John R. Carlson and Scott C. Asbury.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

Dynamic response of NASA rotor test apparatus and Sikorsky S-76 hub mounted in the 80- by 120-foot wind tunnel [microform] / Randall L. Peterson, Muhammed S. Hoque.

Text

Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

A shadowgraphic study of the national launch system's 1 1/2 stage vehicle configuration and heavy lift launch vehicle configuration [microform] / Darlene C. Pokora and Anthony M. Springer.

Text

Marshall Space Flight Center : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

A study of Dean vortex development and structure in a curved rectangular channel with aspect ratio of 40 at Dean numbers up to 430 [microform] / Philip M. Ligrani.

Text

[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Cleveland, Ohio] ; U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1994.

1994

0 resources

Control of wind tunnel operations using neural net interpretation of flow visualization records [microform] / Alvin E. Buggele and Arthur J. Decker.

Text

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

1994

0 resources

Laser transit anemometer measurements on a slender cone in the Langley unitary plan wind tunnel [microform] / William M. Humphreys, Jr. ... [et al.].

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]

1990

0 resources

Close-range photogrammetric measurement of static defections for an aeroelastic supercritical wing [microform] / Thomas A. Byrdsong, Richard R. Adams, and Maynard C. Sandford

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

0 resources

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

0 resources

Some buffet response characteristics of a twin-vertical-tail configuration [microform] / Stanley R. Cole, Steven W. Moss, and Robert V. Doggett.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]

1990

0 resources

Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing [microform] / Paul A. Mirick, M-Nabil H. Hamouda, William T. Yeager.

Text

[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.

1990

0 resources

Simulated rotor test apparatus dynamic characteristics in the 80- by 120-foot wind tunnel [microform] / M.S. Hoque, R.L. Peterson, and T.A. Graham.

Text

Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]

1990

0 resources

Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.

Text

Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.

1991

0 resources

The effect of swirl recovery vanes on the cruise noise of an advanced propeller [microform] / James H. Dittmar and David G. Hall.

Text

[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]

1990

0 resources

Noise measurements from an ejector suppressor nozzle in the NASA Lewis 9- by 15-foot low speed wind tunnel [microform] / Eugene A. Krejsa ... [et al.].

Text

[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]

1990

0 resources

Measured and predicted shock shapes for AFE configuration at mach 6 in air and in FD₄ [microform] / William L. Wells, Alan M. Franks.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]

1988

0 resources

Contraction design for small low-speed wind tunnels [microform] / J.H. Bell, R.D. Mehta ; prepared by Ames Research Center under Cooperative Agreement NCC-2-294.

Text

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, distributor, 1988]

1988

0 resources

Hot-jet simulation in cryogenic wind tunnels [microform] / Keisuke Asai.

Text

[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.

1989

0 resources

Two experimental supercritical laminar-flow-control swept-wing airfoils [microform] / Dennis O. Allison and J. Ray Dagenhart.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]

1987

0 resources

Wind tunnel pressure study and Euler code validation of a missile configuration with 77̊ swept delta wings at supersonic speeds [microform] / Patsy S. Fulton.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]

1988

0 resources

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