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  • Designed for the kill : the jet fighter, development & experience / Mike Spick.

    • Text
    • Shrewsbury, England : Airlife Pub. Ltd., 1995.
    • 1995
    • 1 Item
    FormatCall NumberItem Location
    Text JFF 96-2252Schwarzman Building - Main Reading Room 315
    Request for On-site UseRequest Scan

    Available - Can be used on site. Please visit New York Public Library - Schwarzman Building to submit a request in person.

  • Modern fighter aircraft : technology and tactics : into combat with today's fighter pilots / Anthony Thornborough.

    • Text
    • Sparkford : Patrick Stephens, 1995.
    • 1995
    • 1 Item
    FormatCall NumberItem Location
    Text JSE 96-341Offsite

  • An assessment of viscous effects in computational simulation of benign and burst vortex flows on generic fighter wind-tunnel models using TEAM code [microform] / Tim A. Kinard, Brenda W. Harris, and Pradeep Raj.

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

  • Aerodynamics of the Viggen 37 aircraft. Part 1, General -characteristics at low speed [microform] / Krister Karling.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • 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

  • Effect of emerging technology on a convertible, business/interceptor, supersonic-cruise jet / F.L. Beissner ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Performance study for inlet installations [microform] / D.C. Bingaman.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Investigation into the impact of agility in conceptual fighter design [microform] / R.M. Engelbeck.

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

  • Integrated helmet mounted display concepts for air combat [microform] / Joseph W. Clark.

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

  • Moving base simulation of an ASTOVL Lift-fan aircraft [microform] / William W.Y. Chung, Paul F. Borchers, and James A. Franklin.

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

  • Lateral-directional eigenvector flying qualities guidelines for high performance aircraft [microform] / John B. Davidson, Dominick Andrisani, II.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft [microform] / James A. Franklin.

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

  • Utilization of an agility assessment module in analysis and optimization of preliminary fighter configuration [microform] / Angelen Ngan, Daniel Biezad.

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

  • Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 60̕ half-angle chine forebody [microform] / Holly M. Ross and Matthew J. O'Rourke.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • The F/A-18 high-angle-of-attack ground-to-flight correlation [microform] : lessons learned / Daniel W. Banks ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Closed-loop system identification experience for flight control law and flying qualities evaluation of a high performance fighter aircraft [microform] / Patrick C. Murphy.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data [microform] / Vladislav Klein and Patrick C. Murphy.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Reynolds number effects at high angles of attack [microform] / David F. Fisher ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • 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

  • Euler technology assessment for preliminary aircraft design [microform] : unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration / Todd R. Michal.

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

  • Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models [microform] / Eric F. Charlton.

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

  • A control law design method facilitating control power, robustness, agility, and flying qualities tradeoffs, CRAFT [microform] / Patrick C. Murphy and John B. Davidson.

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

  • Robust, decoupled, flight control design with rate saturated actuators [microform] / S.A. Snell and R.A. Hess.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane [microform] / Frederick J. Lallman, John B. Davidson, and Patrick C. Murphy.

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

  • Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack [microform] / Dale R. Satran, William P. Gilbert, and Ernie L. Anglin.

    • 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

  • Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 [microform] / Francis J. Capone and E. Ann Bare, Dorothy Arbiter.

    • 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

  • Candidate control design metrics for an agile fighter [microform] / Patrick C. Murphy, Melvin L. Bailey, Aaron J. Ostroff.

    • 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
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60321

  • Integrated flight/propulsion control system design based on a decentralized, hierarchical approach [microform] / Duane Mattern and Sanjay Garg, and Randy Bullard.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62070

  • The implementation and operation of a variable-response electronic throttle control system for a TF-104G aircraft [microform] / Bradford Neal and Upal Sengupta.

    • 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, 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69418

  • Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept [microform] / Donald R. Riley and Gautam H. Shah, Richard E Kuhn.

    • 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/LPS72303

  • Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration [microform] / Jay M. Brandon.

    • 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

  • Development and analysis of a STOL supersonic cruise fighter concept [microform] / Samuel M. Dollyhigh, ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Flight test experience with pilot-induced-oscillation suppression filters [microform] / Mary F. Shafer, ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • Calculation of vertical and ramp-assisted takeoffs for supersonic cruise fighters [microform] / Grace C. Liu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Assessment of aerodynamic performance of V/STOL and STOVL fighter aircraft [microform] / W. P. Nelms.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS95844

  • X-29 flight-research program [microform] / Terrill W. Putnam.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • Computer sizing of fighter aircraft [microform] / Peter G. Coen and Willard E. Foss, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Some fighter aircraft trends [microform] / M. Leroy Spearman.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Advances in composites technology [microform] / Darrel R. Tenney and H. Benson Dexter.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • The role of a real-time flight support facility in flight research programs [microform] / Archie L. Moore.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
    • 1986

  • Aerodynamic parameters of an advanced fighter aircraft estimated from flight data : preliminary results / Vladislav Klein, Kevin P. Breneman, Thomas P. Ratvasky.

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS108722

  • Aerodynamic parameters of an advanced fighter aircraft estimated from flight data [microform] : preliminary results / Vladislav Klein, Kevin P. Breneman, Thomas P. Ratvasky.

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

  • Feasibility and benefits of laminar flow control on supersonic cruise airplanes [electronic resource] / A.G. Powell, S. Agrawal, T. R. Lacey.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113610

  • Feasibility and benefits of laminar flow control on supersonic cruise airplanes [microform] / A.G. Powell, S. Agrawal, T. R. Lacey.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113610

  • Flight propulsion control integration for V/STOL aircraft [microform] / James R. Mihaloew ; prepared for the International Powered Lift Conference ; sponsored by the Society of Automotive Engineers, Santa Clara, California, December 7-10, 1987.

    • Text
    • [Washington, D.C.?] : NASA, [1987]
    • 1987

  • Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I : final report / M. R. Mraz, P .E. Hiley.

    • Text
    • St. Louis, Mo. : McDonnell Aircraft Company ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I / M.R. Mraz, P.E. Hiley.

    • Text
    • St. Louis, Missouri : McDonnell Aircraft Company ; Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 1985.
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo34805

  • Computer-automated opponent for manned air-to-air combat simulations / Walter W. Hankins III.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1979.
    • 1979-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52188

  • Pseudosteady-state analysis of nonlinear aircraft maneuvers / John W. Young, Albert A. Schy, and Katherine G. Johnson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71349

  • Air war Italy, 1944-45 : the Axis air forces from the liberation of Rome to the surrender / Nick Beale, Ferdinando D'Amico, Gabriele Valentini.

    • Text
    • Shrewsbury : Airlife, 1996.
    • 1996
    • 1 Item
    FormatCall NumberItem Location
    Text D792.I8 B43 1996gOff-site

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