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  • Flush airdata sensing (FADS) system calibration procedures and results for blunt forebodies [microform] / Brent R. Cobleigh ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • 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

  • Numerical analysis of tangential slot blowing on a generic chined forebody [microform] / Roxana M. Agosta.

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

  • 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

  • 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

  • Experimental aerothermodynamic research of hypersonic aircraft [microform] : technical progress report (substitution) for the period October 1, 1988 - March 31, 1989 / prepared by Eloret Institute ... Joseph W. Cleary, principal investigator.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va.? : National Technical Information Service, distributor, 1989]
    • 1989

  • 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

  • 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, 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

  • Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data [microform] / Michael D. Messina.

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

  • Convective and radiative heating for vehicle return from the Moon and Mars [microform] / R.B. Greendyke, P.A. Gnoffo.

    • 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

  • 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

  • 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

  • A computational examination of directional stability for smooth and chined forebodies at High-α [microform] / Ramakrishnan Ravi and William H. Mason.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
    • 1992

  • Experimental and computational aerothermodynamics of a Mars entry vehicle [microform] / by Brian R. Hollis.

    • Text
    • Raleigh, N.C. : Aerospace Engineering Hypersonic Aerothermodynamics : [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

  • An overview of the NASA F-18 High Alpha Research Vehicle [microform] / Albion H. Bowers ... [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], 1996.
    • 1996

  • Effect of curvature on the impact damage characteritiscs and residual strength of composite plates [microform] / Damodar R. Ambur and James H. Starnes, Jr.

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

  • Effects of chemistry on blunt-body wake structure [microform] / V.K. Dogra ... [et al.].

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

  • Forebody flow visualization on the F-18 HARV with actuated forebody strakes [microform] / David F. Fisher and Daniel G. Murri.

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

  • Experiments in aircraft roll-yaw control using forebody tangential blowing [microform] / Nelson Pedreiro.

    • Text
    • [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Real-time method for estimating viscous forebody drag coefficients [microform] / Stephen A. Whitemore ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, Va. : National Technical Information Service [distributor, 2000]
    • 2000

  • Wind code application to external forebody flowfields with comparisons to experimental results [microform] / F.C. Frate, H.D. Kim.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26734

  • Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack [microform] / Brent R. Cobleigh, Mark A. Croom.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS30134

  • Optimum shape of a blunt forebody in hypersonic flow [microform] / L. Maestrello, L. Ting.

    • Text
    • Hampton, Va. : NASA Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58433

  • Hi-alpha forebody design [microform] / by William H. Mason and R. Ravi.

    • Text
    • Blacksburg, VA : Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration, 1992-
    • 1992-present

  • Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows [microform] : progress report for the period ended December 31, 1989 / by D. J. Singh and S. N. Tiwari ; prepared for National Aeronautics and Space Administration, Langley Research Center.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS63194

  • Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel [microform] / Paul M. Siemers, III and Martin W. Henry.

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

  • Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel [microform] / Paul M. Siemers, III, Martin W. Henry.

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

  • Inlet flowfield investigation. Part II.. Computation of the flow about a supercruise forebody at supersonic speeds [microform].

    • Text
    • Seattle, Wash. : Boeing Military Airplane Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Supersonic retropropulsion test 1853 in NASA LaRC Unitary Plan Wind Tunnel test section 2 / Scott A. Berry and Matthew N. Rhode.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2014.
    • 2014-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54425

  • The F/A-18 high-angle-of-attack ground-to-flight correlation, lessons learned / Daniel W. Banks [and six others].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, January 1997.
    • 1997-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65688

  • Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack / Brent R. Cobleigh, Mark A. Croom.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, May 2001.
    • 2001-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS30134

  • Wind code application to external forebody flowfields with comparisons to experimental results / F.C. Frate, H.D. Kim.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2001.
    • 2001-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS26734

  • Effects of forebody geometry on subsonic boundary-layer stability / S. S. Dodbele.

    • 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

    https://purl.fdlp.gov/GPO/LPS60902

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