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  • Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds [microform] / Robert L. Stallings, Jr., Floyd K. Wilcox, Jr., and Dana K. Forrest.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991

  • Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20 [microform] / Odis C. Pendergraft, Jr., James R. Burley and E. Ann Bare.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.? : National Technical Information Service [distributor], 1986.
    • 1986

  • A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft [microform] / Lisa J. Bjarke, John H. Del Frate, and David F. Fisher.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992

  • Correlation of forebody pressures and aircraft yawing moments on the X-29A aircraft at high angles of attack [microform] / David F. Fisher, David M. Richwine, and Stephen Landers.

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

  • An experimental study of fluctuating pressure loads beneath swept shock/boundary layer interactions [microform] / by Gary S. Settles; principal investigator.

    • Text
    • University Park, PA : Dept. of Mechanical Engineering, Penn State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades [microform] / Aditi Chattopadhyay, Y. Danny Chiu.

    • 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], 1990.
    • 1990

  • PDSS/IMC CIS users guide [microform] / prepared by Intermetrics, Inc.

    • Text
    • Huntsville, Ala. : Intermetrics, Inc. ; [Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Cost-effective design and operation of variable speed wind turbines : closing the gap between the control engineering and the wind engineering community / David-Pieter Molenaar.

    • Text
    • Delft, the Netherlands : Delft University Press, c2003.
    • 2003
    • 1 Item
    FormatCall NumberItem Location
    Text JSE 03-516Offsite

  • Geometrical and structural properties of an aeroelastic research wing (ARW-2) / Maynard C. Sandford ... [et al.].

    • 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, 1989.
    • 1989
    • 1 Item
    FormatCall NumberItem Location
    Text JBX Q-1187Offsite

  • Analysis of aerodynamic coefficients using gust gradient data [microform] : spanwise turbulence effects on airplane response / Erik A. Ringnes and Walter Frost.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by National Technical Information Service, 1986.
    • 1986

  • Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds [microform] / E.B. Plentovich, Julio Chu, and M.B. Tracy.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67795

  • Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate at a Mach number of 5 [microform] / Tony L. Parrott, Michael G. Jones, Cindy W. Albertson.

    • 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], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68643

  • Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes [microform] / James S. Bowman, Jr., Randy S. Hultberg, Colin A. Martin.

    • 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], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68623

  • In-flight investigation of shuttle tile pressure orifice installations [microform] / Timothy R. Moes and Robert R. Meyer, Jr.

    • 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, 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS73726

  • Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel [microform] / Paul M. Siemers, III and Martin W. Henry.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986

  • Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel [microform] / Paul M. Siemers, III, Martin W. Henry.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986

  • Loads and motions of an F-106B flying through thunderstorms [microform] / Roger M. Winebarger.

    • 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

  • Specification for a Program for an Interative Aeroelastic Solution (PIAS) [microform] / Marjorie E. Manro ... [et al.].

    • Text
    • Seattle, Wash. : Boeing Commercial Airplane Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983

  • Numerical analysis of the first static calibration of the RSRA helicopter active-isolator rotor balance system [microform] / C.W. Acree, Jr.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads [microform] / John T. Batina.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96402

  • Detailed pressure distribution measurements obtained on several configurations of an aspect-ratio-7 variable twist wing [microform] / G. Thomas Holbrook and Dana Morris Dunham.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96449

  • Airloads on bluff bodies, with application to the rotor-induced downloads on tilt-rotor aircraft [microform] / W. J. McCroskey, ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; St. Louis, Mo. : United States Army Aviation Research and Development Command, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99887

  • Wind tunnel tests of parabolic trough solar collectors, March 2001- August 2003 / N. Hosoya ... [and others].

    • Text
    • Golden, Colo. : National Renewable Energy Laboratory, [2008]
    • 2008
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS106874

  • Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers / Robert S. Green, George T. Carson, Jr.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
    • 1987
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112156

  • CCBLADE documentation / S.A. Ning.

    • Text
    • Golden, CO : National Renewable Energy Laboratory, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49548

  • An unsteady lifting surface method for single rotation propellers / Marc H. Williams.

    • 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, 1990.
    • 1990
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60897

  • Jian zhu jie gou yu feng he zai / Zhang Peixin bian zhu.

    • Text
    • Shanghai : Shanghai ke xue ji shu chu ban she, 2013.
    • 2013
    • 1 Item
    FormatCall NumberItem Location
    Text TA654 .Z43 2013Off-site

  • Prop-fan integration / Ioannis C. Theocleous.

    • Text
    • [S.l. : s.n.], c1995.
    • 1995
    • 1 Item
    FormatCall NumberItem Location
    Text TL571 .T430 1995qOff-site

  • Manual on aircraft loads, by James Taylor.

    • Text
    • Oxford, New York, Published for and on behalf of Advisory Group for Aeronautical Research and Development, North Atlantic Treaty Organization by Pergamon Press [c1965]
    • 1965
    • 1 Item
    FormatCall NumberItem Location
    Text 92513.896Off-site

  • The peak pressure rise across an oblique shock emerging from a turbulent boundary layer over a plane surface / by Luigi Crocco and Ronald F. Probstein. [Sponsored jointly by the] United States and [the] United States Air Force, Office of Scientific Research.

    • Text
    • [S.L. : s.n.], 1954.
    • 1954
    • 1 Item
    FormatCall NumberItem Location
    Text 92515.275Off-site

  • Atmospheric turbulence environment with special reference to continuous turbulence.

    • Text
    • [Paris, North Atlantic Treaty Organization, 1957]
    • 1957
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-115Off-site

  • A relation between measured c.g. vertical accelerations and the loads at the t-tail of a military airplane, by O. Buxbaum.

    • Text
    • [Neuilly-sur-Seine, France] North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development [1972]
    • 1972
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-597Off-site

  • Critical flight conditions and loads resulting from inertial cross-coupling and aerodynamic stability deficiencies / by W.J.G. Pinsker.

    • Text
    • Paris : North Atlantic Treaty Organization, 1957.
    • 1957
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-107Off-site

  • Flight loads measurements on NACA research airplanes / by De E. Beeler.

    • Text
    • Paris : North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, [1957]
    • 1957
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-109Off-site

  • Unsteady viscous thin airfoil theory / by J.E. Yates.

    • Text
    • Neuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1979.
    • 1979
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-671Off-site

  • Investigation of unsteady airloads on wings with oscillating control for active control purposes / by W. Geissler.

    • Text
    • Neuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1981.
    • 1981
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-699Off-site

  • Operational loads measurement and evaluation.

    • Text
    • Neuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development ; Springfield, Va., USA : National Technical Information Service [distributor], 1982.
    • 1982
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-703Off-site

  • Unsteady pressures due to control surface rotation at low supersonic speeds : comparison between theory and experiment / by C.G. Lodge and H. Schmid.

    • Text
    • 1976
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-647Off-site

  • Combat loads on modern fighters.

    • Text
    • Neuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1986.
    • 1986
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-730Off-site

  • Some aspects of aircraft dynamic loads due to flow separation / by D.G. Mabey.

    • Text
    • Neuilly-sur-Seine, France : AGARD, 1988.
    • 1988
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-750Off-site

  • Aircraft loads due to turbulence and their impact on design and certification = Efforts avion dus à la turbulence atmosphérique et leurs impacts sur la conception et la certification

    • Text
    • Neuilly sur Seine, France: North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1994.
    • 1994
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-798Off-site

  • Extreme value analysis and its application to c.g. vertical accelerations measured on transport airplanes of type C-130 [Texte imprimé] / by Otto Buxbaum.

    • Text
    • Neuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development ; [Springfield, Va. : Available from the National Technical Information Service], 1971.
    • 1971
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-579-71Off-site

  • A method for the prediction of the onset of buffeting and other separation effects from wind tunnel tests on rigid models / by H.H. Pearcey.

    • Text
    • Paris : North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, 1958.
    • 1958
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-223Off-site

  • Prop-fan integration / Ioannis C. Theocleous.

    • Text
    • [S.l. : s.n.], c1995.
    • 1995
    • 1 Item
    FormatCall NumberItem Location
    Text TL571 .T430 1995q OversizeOff-site

  • Manual on aircraft loads, by James Taylor.

    • Text
    • Oxford, New York, Published for and on behalf of Advisory Group for Aeronautical Research and Development, North Atlantic Treaty Organization, by Pergamon Press [©1965]
    • 1965
    • 1 Item
    FormatCall NumberItem Location
    Text 92513.896Off-site

  • A relation between measured c.g. vertical accelerations and the loads at the t-tail of a military airplane / by O. Buxbaum (Laboratorium für Betriebsfestigkeit 61 Darmstadt-Eberstadt Mühltalstrasse 55, West Germany).

    • Text
    • [Neuilly-sur-Seine, France] : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1972.
    • 1972
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-597Off-site

  • Unsteady pressures due to control surface rotation at low supersonic speeds : comparison between theory and experiment / by C.G. Lodge and H. Schmid.

    • Text
    • Neuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1976.
    • 1976
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-647Off-site

  • Combat loads on modern fighters.

    • Text
    • Neuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1986.
    • 1986
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-730Off-site

  • Some aspects of aircraft dynamic loads due to flow separation / by D.G. Mabey.

    • Text
    • Neuilly-sur-Seine, France : AGARD, 1988.
    • 1988
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-750Off-site

  • A method for the prediction of the onset of buffeting and other separation effects from wind tunnel tests on rigid models / by H.H. Pearcey.

    • Text
    • Paris : North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, 1958.
    • 1958
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-223Off-site

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