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  • Navier-Stokes simulation of several high-lift reference H configurations [microform] / Wendy B. Lessard.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study [microform] / C. Frederic Smith and Steve D. Podleski.

    • Text
    • [Cleveland, Ohio] : Lewis Research Center ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • An experimental study of the flowfield on a semispan rectangular wing with a simulated glaze ice accretion [microform] / Abdollah Khodadoust.

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

  • Control of low-speed turbulent separated flow over a backward-facing ramp [microform] / by John C. Lin.

    • Text
    • [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 leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds [microform] / Gloria Hernandez ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept [microform] / Bandu N. Pamadi.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • F/A-18 forebody vortex control [microform] / Brian R. Kramer ... [et al.].

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

  • Water tunnel flow visualization study of a 4.4% scale X-31 forebody [microform] / Brent R. Cobleigh and John Del Frate.

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

  • Effects of vibration on inertial wind-tunnel model attitude measurement devices [microform] / Clarence P. Young, Jr. ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test [microform] / Brent R. Cobleigh.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Computational analysis of forebody tangential slot blowing on the high alpha research vehicle [microform] / Ken Gee.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model [microform] / Stacey J. Cotton and Lisa J. Bjarke.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Research in robust control for hypersonic vehicles [microform] : progress report #1 / principal investigator: A.J. Calise.

    • Text
    • Atlanta, Ga. : School of Aerospace Engineering, Georgia Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • A preliminary look at techniques used to obtain airdata from flight at high angles of attack [microform] / Timothy R. Moes and Stephen A. Whitmore.

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

  • Prediction of the noise from a propeller at angle of attack [microform] / Eugene A. Krejsa.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Wind tunnel pressure study and Euler code validation of a missile configuration with 77̊ swept delta wings at supersonic speeds [microform] / Patsy S. Fulton.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Numerical simulation of the flow about the F-18 HARV at high angle of attack [microform] / Scott M. Murman.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack [microform] / Crawford F. Smith.

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

  • Fourth High Alpha Conference, NASA Dryden Flight Research Center, Edwards, California, July 12-14, 1994 [microform]

    • 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], 1994.
    • 1994

  • 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall [microform] / R.A. Piziali.

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

  • 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

  • Wing pressure distributions from subsonic tests of a high-wing transport model [microform] / Zachary T. Applin and Carl L. Gentry, Jr., M.A. Takallu.

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

  • Computation of asymmetric supersonic flows around cones at large incidence [microform] : final report / principal investigator, David Degani.

    • Text
    • Technion City, Haifa, Israel : Technion Research & Development Foundation ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987?]
    • 1987

  • 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

  • Computations and turbulent flow modeling in support of helicopter rotor technology [microform] / by William C. Rose.

    • Text
    • Reno, NV : Engineering Research and Development Center, University of Nevada ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Experimental analyses of trailing edge flows [microform] : final technical report to NASA Ames Research Center / S.L. Petrie, D.S. Emmer.

    • Text
    • [Moffett Field, Calif.] : The Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986?]
    • 1986

  • Rotary balance data and analysis for the X-29A airplane for an angle-of-attack range of 0⁰ to 90⁰ [microform] / John N. Ralston.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1984.
    • 1984

  • Low speed rotary aerodynamics of F-18 configuration for 0⁰ to 90 ⁰ angle of attack [microform] : test results and analysis / Randy Hultberg.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1984.
    • 1984

  • Numerical simulation of the flow about the F-18 HARV at high angle of attack [microform] / Scott M. Murman.

    • Text
    • San Jose, CA : MCAT Institute ; [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

  • Experimental study of the effects of reynolds number on high angle of attack aerodynamic characteristics of forebodies during rotary motion [microform] / H. Pauley, J. Ralston, and E. Dickes.

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

  • Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching [microform] / J. Moreira and H. Johari.

    • Text
    • Worcester, MA : Mechanical Engineering Dept., Worcester Polytechnic Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Numerical simulation of the flow about the F-18 HARV at high angle of attack [microform] / Scott M. Murman.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept [microform] / B. Spencer, Jr., C.H. Fox, Jr., and J.K. Huffman.

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

  • Evaluation of F/A-18A HARV inlet flow analysis with flight data [microform] / C. Frederic Smith ... [et al.].

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

  • F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness [microform] / Eugene A. Morelli.

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

  • Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes [microform] / Gregory M. Catlin, Brian E. McGrath.

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

  • A study of large droplet ice accretion in the NASA Lewis IRT at near-freezing conditions; Pt. 2 [microform] / Harold E. Addy, Jr. and Dean R. Miller, Robert F. Ide.

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

  • 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

  • Three dimensional solution of pneumatic active control of forebody vortex asymmetry [microform] / Osama A. Kandil and Hazem H. Sharaf El-Din, C.H. Liu.

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

  • Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach [microform] / W.P. Norby, J.A. Ladd, and A.J. Yuhas.

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

  • 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

  • Final report on study of organized structures in the post-stall flow over wings [microform] / Steven Yon; Joseph Katz, principal investigator; James Ross, principal investigator.

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

  • Computational investigation of tangential slot blowing on a generic chined forebody [microform] / Roxana M. Agosta-Greenman ... [et al.].

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

  • Design specification for a thrust-vectoring, actuated-nose-strake flight control law for the high-alpha research vehicle [microform] / Barton J. Bacon ... [et al.].

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

  • 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

  • Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions [microform] / Robert E. Bartels and John W. Edwards.

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

  • A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 [microform] / Richard J. Re and William K. Abeyounis.

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

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