Research Catalog

  • A flying qualities study of longitudinal long-term dynamics of hypersonic planes [microform] / Timothy H. Cox ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995
  • 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
  • NASA/FAA Tailplane Icing Program [microform] : flight test report / Thomas P. Ratvasky, Judith Foss Van Zante, Alex Sim.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 2000]
    • 2000
  • Determining the accuracy of maximum likelihood parameter estimates with colored residuals [microform] / Eugene E. Morelli, Vladislav Klein.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Application of parameter estimation to highly unstable aircraft [microform] / Richard E. Maine and James E. Murray.

    • 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], 1986.
    • 1986
  • Launch vehicle flight dynamics [microform] : final report under contract NAS8-39131, delivery order no. 27 / submitted by Auburn University, College of Engineering and Engineering Experiment Station, Department of Aerospace Engineering.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Cooperative control theory and integrated flight and propulsion control [microform] : final technical report for grant NAG3-575 covering the period 1994-1995 / prepared by David K. Schmidt and John D. Schierman.

    • Text
    • College Park, Md. : Dept. of Aerospace Engineering, University of Maryland ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Launch vehicle flight dynamics [microform] : final report under contract NAS8-39131, delivery order no. 27 / submitted by Auburn University, College of Engineering and Engineering Experiment Station, Department of Aerospace Engineering.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • PREDAVOR [microform] : development and implementation of software for rapidly estimating aircraft stability derivatives and handling qualities : a thesis ... / by Danielle Suzanne Soban.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; 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
  • Estimation of aircraft nonlinear unsteady parameters from wind tunnel data [microform] / Vladislav Klein, Patrick C. Murphy.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Relative control effectiveness technique with application to airplane control coordination [microform] / Frederick J. Lallman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service,] 1985.
    • 1985
  • Characterizing the severe turbulence environments associated with commercial aviation accidents [microform]. Part I, 44 case study synoptic observational analyses / Michael L. Kaplan ... [et al.].

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60163
  • A historical overview of flight flutter testing [microform] / Michael W. Kehoe.

    • 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, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60729
  • An aerodynamic tradeoff study of the scissor wing configuration [microform] / Bruce P. Selberg, Kamran Rokhsaz, Clinton S. Housh.

    • Text
    • Rolla, Mo. : University of Missouri-Rolla ; [Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS63191
  • Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring" [microform] : June 11, 1989-December 10, 1989 / by J.B. Tseng and C. Edward Lan.

    • Text
    • Lawrence, Kan. : Flight Research Laboratory, University of Kansas Center for Research ; [Washington, D.C. : National Aeronautics and Space Administration, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69319
  • The measurement of aircraft performance and stability and control after flight through natural icing conditions [microform] / Richard J. Ranaudo ... [et al.].

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986
  • Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data [microform] / Robert Alan Hess.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85279
  • Bifurcation analysis of aircraft pitching motions near the stability boundary [microform] / W.H. Hui and Murray Tobak.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984
  • A Lagrange-D'Alembert forumulation of the equations of motion of a helicopter carrying an externally suspended load [microform] / Jeanine M. Weber and Richard K. Greif.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96096
  • Integrated structure/control law design by multilevel optimization / Michael G. Gilbert, David K. Schmidt.

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS108705
  • Integrated structure/control law design by multilevel optimization [microform] / Michael G. Gilbert, David K. Schmidt.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
  • Study on using a digital ride quality augmentation system to trim an engine-out in a Cessna 402B [microform] / by: Kent E. Donaldson.

    • Text
    • Lawrence, Kan. : University of Kansas Center for Research, Inc., Flight Research Laboratory, [1986?]
    • 1986
  • Dependence of dynamic modeling accuracy on sensor measurements, mass properties, and aircraft geometry / Jared A. Grauer and Eugene A. Morelli.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2013.
    • 2013-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50504
  • Artificial intelligence based control power optimization on tailless aircraft : ARMD seedling fund, phase I, final report / Frank H. Gern [and seven others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2014.
    • 2014-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo59317
  • User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation / Richard E. Maine and Kenneth W. Iliff.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
    • 1980-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70968
  • A flying qualities study of longitudinal long-term dynamics of hypersonic planes / Timothy H. Cox [and three others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Facility, April 1995.
    • 1995-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82735
  • Simulator evaluation of displays for a revised takeoff performance monitoring system / David B. Middleton, Raghavachari Srivatsan, and Lee H. Person, Jr.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1992.
    • 1992-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo150746
  • Synthesis from design requirements of a hybrid system for transport aircraft longitudinal control / Charles S. Hynes and Gordon H. Hardy, Lance Sherry.

    • Text
    • Moffett Field, Calif. : National Aeronautics and, Space Administration, Ames Research Center, [2007]
    • 2007
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33400
  • Flight test results on the stability and control of the F-15 Quiet Spike aircraft / Cheng M. Moua [and three others].

    • Text
    • Edwards, CA : National Aeronautics and, Space Administration, Dryden Flight Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32721
  • A note on multicyclic control by swashplate oscillation / James C. Biggers and John L. McCloud, III.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 1978.
    • 1978
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo152415
  • Analogy between the Collatz Conjecture and sliding mode control / Jared A. Grauer.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2021.
    • 2021-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo171607
  • In-flight turbulence emulation for fixed-wing aircraft using equivalent multisine excitations / Jared A. Grauer.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2021.
    • 2021-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo171822
  • The implications of handling qualities in civil helicopter accidents involving hover and low speed flight / Daniel C. Dugan and Kevin J. Delamer.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, November 2005.
    • 2005-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo172632
  • Simulation and evaluation of SH-2F helicopter in a shipboard environment using the interchangeable cab system / Clyde H. Paul, David L. Astill, and Shawn T. Donley.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, August 1983.
    • 1983-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo172630
  • Exploratory investigation of the incipient spinning characteristics of a typical light general aviation airplane / by Richard J. Ranaudo.

    • Text
    • [Washington, D.C.] : [National Aeronautics and Space Administration], [January 1977]
    • 1977-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173914
  • Worst-case flutter margins from F / A-18 aircraft aeroelastic data / Rick Lind, Marty Brenner.

    • Text
    • [Washington, D.C.] : [National Aeronautics and Space Administration], [April 1997]
    • 1997-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo174938
  • Research in robust control for hypersonic aircraft : progress report #2, 1 December 1992- 31 August 1993 / principal investigator: A.J. Calise.

    • Text
    • [Washington, D.C.] : [National Aeronautics and Space Administration], October 1993.
    • 1993-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo176341

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta