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  • A comparison of experimental and theoretical results for labyrinth gas seals with honeycomb stators [microform] / by Lawrence Allen Hawkins.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • A study of rotor broadband noise mechanisms and helicopter tail rotor noise [microform] / Shau-Tak Rudy Chou.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Computation of helicopter rotor acoustics in forward flight [microform] / Roger Strawn, Rupak Biswas.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Coupled 2-dimensional cascade theory for noise and unsteady aerodynamics of blade row interaction in turbofans. Volume 1, Theory development and parametric studies [microform] / Donald B. Hanson.

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

  • Measurements of atmosopheric turbulence effects on tail rotor acoustics [microform] / Martin J. Hagen ... [et al.].

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

  • Aeroelastic simulation of higher harmonic control [microform] / Lawson H. Robinson and Peretz P. Friedmann.

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

  • Flutter analysis of supersonic axial flow cascades using a high resolution euler solver. Part 1, Formulation and validation [microform] / T.S.R. Reddy ... [et al.].

    • Text
    • Washington, DC : National Aeronautics and Space Administration, [1992]
    • 1992

  • Computational fluid dynamics study of the variable-pitch split-blade fan concept [microform] / C.E. Kepler, A.R. Elmquist and R.L. Davis.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • A review of ice accretion data from a model rotor icing test and comparison with theory [microform] / Randall K. Britton.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades [microform] / J.D. Baeder.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation Systems Command, Aviation Research and Technology Activity ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1991]
    • 1991

  • A study of helicopter stability and control including blade dynamics [microform] / Xin Zhao, H.C. Curtiss, principal investigator.

    • Text
    • [Princeton, N.J.] : Princeton University, Dept. of Mechanical nad Aerospace Engineering ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Dynamics of the McDonnell Douglas large scale dynamic rig and dynamic calibration of the rotor balance [microform] / Khanh Nguyen and Benton Lau.

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

  • Measurement of gust response on a turbine cascade [microform] : / A.P. Kurkov and B.L. Lucci.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Experimental study of unsteady hydrodynamic force matrices on whirling centrifugal pump impellers [microform] / Belgacem Jery.

    • Text
    • Pasadena, Calif. : California Institute of Technology ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor], 1986.
    • 1986

  • Implementation and validation of a wake model for vortex-surface interactions in low-speed forward flight [microform] : semi-annual status report, period 10/1/86 - 3/31/87 / Narayanan M. Komerath, Olivier A. Schreiber.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • An experimental and analytical method for approximate determination of the tilt rotor research aircraft rotor-wing download [microform] : final report, 05-30-94 - 11-30-85 / principal investigator, David E. Jordan, William Patterson, Doral R. Sandia.

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University, Aeronautical Engineering Dept. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1985

  • Linear and nonlinear dynamic analysis of redundant load path bearingless rotor systems [microform] / V.R. Murthy, principal investigator.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • NASA-Army rotorcraft technology [microform] : proceedings of a conference ... held at Ames Research Center, Moffett Field, California, March 17-19, 1987.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], <1988- >
    • 1988-present
    • 2 Items
    FormatCall NumberItem Location
    Text JSK 88-98 v. 1Offsite
    FormatCall NumberItem Location
    Text JSK 88-98 v. 2Offsite

  • Recent improvements to and validation of the one dimensional NASA wave rotor model [microform] / Daniel E. Paxson and Jack Wilson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Integrated Technology Rotor Methodology Assessment Workshop [microform] : proceedings of a workshop / sponsored by NASA Ames Research Center and the U.S. Army, June 21-22, 1983 ; edited by Michael J. McNulty, William G. Bousman.

    • Text
    • Moffett Field, CA : US Army Aviation Systems Command, Aviation Research and Technology Activity ; [Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.? : National Technical Information Service, distributor], 1988.
    • 1988

  • Development and validation of a blade-element mathematical model for the AH-64A Apache helicopter [microform] / M. Hossein Mansur.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis [microform] / Thomas H. Maier and William G. Bousman.

    • Text
    • Moffett Field, Calif. : US Army Aviation and Troop Command : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Application of a personal computer for the uncoupled vibration analysis of wind turbine blade and counterweight assemblies [microform] / Phillip R. White and Ronald R. Little.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Aeroelastic model helicopter rotor testing in the Langley TDT [microform] / Wayne, R. Mantay ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • A numerical model for dynamic wave rotor analysis [microform] / D.E. Paxson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Aircraft noise prediction program theoretical manual [microform] : rotorcraft system noise prediction system (ROTONET) / Donald S. Weir ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors [microform] : user's manual / James F. Schmidt.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Nonlinear (time domain) and linearized (title & freqency domain) solutions to the compressible Euler equations in conservation law form [microform] : final report for NASA Lewis Research Center / by Kidambi Sreenivas and David L. Whitfield.

    • Text
    • Mississippi States, MS : Computational Fluid Dynamics Laboratory, Engineering Research Center for Computational Field Simulation, Mississippi State University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Full-scale hingeless rotor performance and loads [microform] / Randall L. Peterson.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight [microform] : final technical report under NASA-Ames research grant no. NAG 2-797 / G.H. Gaonkar, S. Subramanian.

    • Text
    • Boca Raton, FL : Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • A survey of theoretical and experimental coaxial rotor aerodynamic research [microform] / Colin P. Coleman.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Computation of loads on the McDonnell Douglas advanced bearingless rotor [microform] / Khanh Nguyen, Dan Lauzon and Vaidyanathan Anand.

    • Text
    • [Mesa, AZ : American Helicopter Society, Inc. ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, c1994]
    • 1994

  • Energy efficient engine low pressure subsystem flow analysis [microform] / Edward J. Hall ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, [distributor, 1998]
    • 1998

  • Aeroacoustic codes for rotor harmonic and BVI noise - CAMRAD.Mod1/HIRES [microform] : methodology and users' manual / D. Douglas Boyd, Jr. ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Three-dimensional flow field measurements in a transonic turbine [microform] / P.W. Giel ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration : U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Source methodology for turbofan noise prediction (SOURCED3D technical documentation) [microform] / Harold D. Meyer.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • On the coupling of CDISC design method with FPX rotor code [microform] / Hong Hu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery [microform] / Robert E. Cunningham.

    • 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

  • Integrated multidisciplinary optimization of rotorcraft [microform] : a plan for development / edited by Howard M. Adelman and Wayne R. Mantay.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989

  • Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack [microform] / M. Nallasamy and J.F. Groeneweg.

    • Text
    • Cleveland, Ohio : Lewis Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58503

  • Experimental determination of gap flow-conditioned forces at turbine stages and their effect on the running stability of simple rotors [microform] / Raimund Wohlrab.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983

  • Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode [microform] / Michael B. Lance, Daniel Y. Sung, Robert H. Stroub.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60324

  • Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets [microform] / Henry L. Kelley.

    • 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/LPS61086

  • A new methodology for free wake analysis using curved vortex elements [microform] / Donald B. Bliss, Milton E. Teske, and Todd R. Quackenbush.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67054

  • Validation of viscous and inviscid computational methods for turbomachinery components [microform] / Louis A. Povinelli.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Rotor performance characteristics from an aeroacoustic helicopter wind-tunnel test program [microform] / Danny R. Hoad, Joe W. Elliott and Nettie M. Orie.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986

  • Rotor/body aerodynamic interactions [microform] / Mark D. Betzina, Charles A. Smith, and Patrick Shinoda.

    • 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

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

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
    • 1983

  • Investigation of flow phenomena in a transonic fan rotor using laser anemometry [microform] / Anthony J. Strazisar.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • Parametric tip effects for conformable rotor applications [microform] / Wayne R. Mantay, William T. Yeager, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983

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