Research Catalog

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  • 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

  • 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

  • Development of a mulicomponent force and moment balance for water tunnel applications [microform] / Carlos J. Suárez ... [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], 1994.
    • 1994

  • Sailplane glide performance and control using fixed and articulating winglets [microform] : a thesis / by James David Colling.

    • 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

  • Roll-yaw control at high angle of attack by forebody tangential blowing [microform] / N. Pedreiro ... [et al.].

    • Text
    • [Stanford, Calif.?] : Joint Institute for Aeronautics and Acoustics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • 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

  • 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

  • Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV [microform] / David F. Fisher, Daniel G. Murri, and Wendy R. Lanser.

    • 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

  • 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

  • Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV / David F. Fisher, Daniel G. Murri, and Wendy R. Lanser.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65675

  • 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

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