Research Catalog

  • 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
  • Subsonic wing optimization for handling qualities using ACSYNT [microform] : final report, MS thesis : NASA grant number NCC 2-855, Cal Poly project 5339 / Dani Soban, [principal investigator], Daniel J. Biezad.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • 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
  • Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight [microform] : interim technical report under NASA-Ames Research grant no. NAG-2-797 (August 1, 1992 - December 21, 1993) / G.H. Gaonkar, S. Subramanian, Srinivas Chunduru.

    • 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, 1994]
    • 1994
  • Analysis of flight data from a high-incidence research model by system identification methods [microform] / James G. Batterson, Vladislav Klein.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1989.
    • 1989
  • Effect of control surface mass unbalance on the stability of a closed-loop active control system [microform] / E. Nissim.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1989.
    • 1989
  • General rotorcraft aeromechanical stability program (GRASP) theory manual [microform] / Dewey H. Hodges ... [et al.].

    • 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, 1990]
    • 1990
  • The aluminum falcon [microform] : a low cost modern commercial transport / Non-Solo Design Group.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method [microform] : progress report / Marcello R. Napolitano.

    • Text
    • Morgantown, WV : West Virginia University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • A spectrally accurate boundary-layer code for infinite swept wings [microform] / C. David Pruett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1994
  • Flight determination of the aerodynamic stability and control characteristics of the NASA SGS 1-36 sailplane in the conventional and deep stall angles-of-attack of between -5 and 75 degrees [microform] / by Faramarz A. Mahdavi, Dral R. Sandlin.

    • 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, 1984]
    • 1984
  • A correlation study of X-29A aircraft and associated analytical development [microform] / by Ali Ahmadi, Kajal Gupta, Paul Fortin.

    • Text
    • Lawrence, Kan. : University of Kansas Center for Research ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988
  • Vortex flap technology [microform] : a stability and control assessment / K.M. Carey and G.E. Erickson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1984
  • Investigation of empennage buffeting [microform] : technical report CRINC-FRL-714-1 / by C. Edward Lan and I.G. Lee, William H. Wentz.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Individual-blade-control research in the MIT VTOL Technology Laboratory 1977-1985 [microform] / Norman D. Ham.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack [microform] : final report / prepared by W.H. Hui.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985
  • 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
  • Interactive aircraft flight control and aeroelastic stabilization [microform] : semi-annual report 1 May 1985 through 31 October 1985 / submitted by Terrence A. Weisshaar.

    • Text
    • West Lafayette, Ind. : School of Aeronautics and Astronautics, Purdue University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985
  • FPCAS3D user's guide [microform] : full potential aeroelastic program / Milind A. Bakhle.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept [microform] / A.M. Springer.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊ [microform] / Scott P. Fears, Holly M. Ross, and Thomas M. Moul.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Performance of a low-power subsonic-arc-attachment arcjet thruster [microform] / John M. Sankovic and Darren H. Berns.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • 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
  • CLMNANAL, a C++ program for application of the Coleman stability analysis to rotorcraft [microform] / Michael B. Lance.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Euler/Navier-Stokes flow computations on flexible configurations for stability analysis [microform] / G. Guruswamy and E. Tu.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1995
  • Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel [microform] / Glen P. Doggett and Ndaona Chokani.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge [microform] : NASA contract no. NAS1-19480 / Peter W. Duck, D. Glenn Lasseigne, M.Y. Hussaini.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Low-speed wind tunnel tests of two waverider configuration models [microform] / Robert J. Pegg, David E. Hahne, Charles E. Cockrell, Jr.

    • Text
    • Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Aeroelastic stability of a full-scale hingeless rotor [microform] / Randall L. Peterson and Khanh Nguyen.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Technical evaluation report on unsteady aerodynamics--fundamentals and applications to aircraft dynamics [microform] / D.G. Mabey and J.R. Chambers.

    • Text
    • [Neuilly-sur-Seine, France] : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development ; [Washington, DC : National Aeronautics and Space Administration, Goddard Space Flight Center ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Direct adaptive aircraft control using dynamic cell structure neural networks [microform] / Charles C. Jorgensen.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Flight stability and control and performance results from the Linear Aerospike SR-71 Experiment (LASRE) [microform] / Timothy R. Moes ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Nonlinear stability of supersonic jets [microform] : final report / by T.R.S. Bhat and S.N. Tiwari, principal investigator ; submitted by the Old Dominion University Research Foundation.

    • Text
    • Norfolk, Va. : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Euler technology assessment [microform] : SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts / Keith J. Jordan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998
  • Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft [microform] / W.G. Steenken ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999
  • Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept [microform] / David E. Hahne.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Aerothermodynamics of the Mars Global Surveyor spacecraft [microform] / Russell W. Shane and Robert H. Tolson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Rotorcraft dynamics 1984 [microform] : proceedings of the 2nd decennial Specialists' Meeting on Rotorcraft Dynamics sponsored by NASA Ames Research Center and the American Helicopter Society and held at NASA Ames Research Center, Moffett Field, California, November 7-9, 1984.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
    • 1985
  • Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops [microform] / Zachary T. Applin and Paul L. Coe, Jr.

    • 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
  • Prediction of forces and moments for flight vehicle control effectors [microform] / M. Maughmer ... [et al.].

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 2 Resources

    Available Online

    See All Available Online Resources

  • The application of active controls technology to a generic hypersonic aircraft configuration [microform] / M.G. Gilbert ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69437
  • Interactive aircraft flight control and aeroelastic stabilization [microform] : semi-annual report 1 November 1984 through 30 April 1985 / submitted by Terrence A. Weisshaar, principal investigator.

    • Text
    • West Lafayette, Ind. : School of Aeronautics and Astronautics, Purdue University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985
  • Transonic calculation of airfoil stability and response with active controls [microform] / J. T. Batina, T. Y. Yang.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984
  • Viscous effects on transonic airfoil stability and response [microform] / H. M. Berry, J. T. Batina, T. Y. Yang.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
  • Potential benefits of magnetic suspension and balance systems / Pierce L. Lawing, David A. Dress, and Robert A. Kilgore.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112209
  • Potential benefits of magnetic suspension and balance systems [microform] / Pierce L. Lawing, David A. Dress, and Robert A. Kilgore.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112209
  • Theory of wing rock [microform] / by Chung-Hao Hsu and C. Edward Lan.

    • Text
    • Hamptan, VA : Langley Research Center, National Aeronautics and Space Administration, [1984]
    • 1984
  • Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed [microform] / by Arthur F. Smith.

    • Text
    • Windsor Locks, Conn. : United Technologies Corporation, Hamilton Standard Division ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
    • 1985
  • Virtual deformation control of the X-56A model with simulated fiber optic sensors / Peter M. Suh and Alexander W. Chin, Dimitri N. Mavris.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, January 2014.
    • 2014-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50964
  • Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / Bobby W. Sanders.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
    • 1980-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52217

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