1–50 of 3,278 hits
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    ZEHST: environmental challenges for hypersonic passenger transport

    Defoort, Sebastien / Serre, Laurent / Grenon, Richard et al. | AIAA | 2012
    Publisher: The American Institute of Aeronautics and Astronautics

      ZEHST: ENVIRONMENTAL CHALLENGES FOR HYPERSONIC PASSENGER TRANSPORT

      Defoort, S. / Serre, L. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012
      Keywords: Space planes , Hypersonic systems

    X-51A Scramjet Engine Flight Demonstration Program

    Mutzman, R. / Murphy, J. / Hank, J. et al. | British Library Conference Proceedings | 2008
    Publisher: AIAA , Reston
    Keywords: Space planes , Hypersonic systems

    X-43D Conceptual Design and Feasibility Study

    Johnson, Donald / Robinson, Jeffrey | AIAA | 2005
    Publisher: The American Institute of Aeronautics and Astronautics

      X-43D Conceptual Design and Feasibility Study

      Johnson, Donald B. / Robinson, Jeffrey S. | NTRS | 2005
      Initiative (NAI), a multi-year, multi-agency cooperative effort to invest in and develop, among other things, hypersonic technologies. This roadmap ...
      Publisher: NASA National Aeronautics and Space Administration
      Keywords: Spacecraft Design, Testing And Performance

    X-43C Plans and Status

    Moses, P. | AIAA | 2003
    Publisher: The American Institute of Aeronautics and Astronautics

      X-43C Plans and Status

      Moses, Paul L. | NTRS | 2003
      X-43C Project is a hypersonic flight demonstration being executed as a collaboration between the National Aeronautics and Space ...
      Publisher: NASA National Aeronautics and Space Administration
      Keywords: Spacecraft Propulsion And Power

    X-43A Vehicle Design and Manufacture

    Harsha, Philip / Keel, Lowell / Castrogiovanni, Anthony et al. | AIAA | 2005
    Publisher: The American Institute of Aeronautics and Astronautics

    X-43A Stage Separation System - A Flight Data Evaluation

    Blocker, Wayne / Ruebush, David | AIAA | 2005
    Publisher: The American Institute of Aeronautics and Astronautics

    X-43A Fluid and Environmental Systems: Ground and Flight Operation and Lessons Learned

    Vachon, Michael / Grindle, Thomas / St. John, Clinton et al. | AIAA | 2005
    Publisher: The American Institute of Aeronautics and Astronautics

    X-43A Fluid and Environmental Systems: Ground and Flight Operation and Lessons Learned

    Vachon, Michael Jacob / Grindle, Thomas J. / St.John, Clinton W. et al. | NTRS | 2005
    fineness ratio resulted in very small internal space available for fluid systems and their corresponding environmental conditioning systems. Safe ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Ground Support Systems And Facilities (Space)

    X-43A Flight-Test-Determined Aerodynamic Force and Moment Characteristics at Mach 7.0

    Davis, Mark C. / White, J. Terry | NTRS | 2008
    airframe-integrated scramjet-powered aircraft in hypersonic flight. These data were gathered via a repeated series of pitch, yaw, and roll doublets ...
    Publisher: NASA National Aeronautics and Space Administration

    X-38 European partnership

    Klaedtke, Ralf / Puettmann, Norbert / Graf, E. | AIAA | 1999
    Publisher: The American Institute of Aeronautics and Astronautics

    X-33-Reusable Launch Vehicle Structural Technologies

    Bechtel, R. / Smith, D. / AIAA | British Library Conference Proceedings | 1996
    Publisher: AIAA
    Keywords: space planes systems , hypersonic systems , AIAA , aerospace plane technologies

    X-33-Reusable Launch Vehicle Propulsion Technology

    Smith, D. / AIAA | British Library Conference Proceedings | 1996
    Publisher: AIAA
    Keywords: space planes systems , hypersonic systems , AIAA , aerospace plane technologies

    Working Process Organization in Rocket-Ramjet with Air Liquefaction Cycle

    Makaron, V. / Fedyayev, Y. / AIAA | British Library Conference Proceedings | 1996
    Publisher: AIAA
    Keywords: space planes systems , hypersonic systems , AIAA , aerospace plane technologies

    Wingtip Vortex Attenuation by Plasma Actuator

    Golub, Victor / Agibalova, Svetlana / Moralev, Ivan et al. | AIAA | 2012
    Publisher: The American Institute of Aeronautics and Astronautics

    Wind tunnel tests for separation dynamics modeling of a two-stage hypersonic vehicle

    Breitsamter, C. / Laschka, B. / Zaehringer, C. et al. | AIAA | 2001
    Publisher: The American Institute of Aeronautics and Astronautics

      Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic Vehicle

      Breitsamter, C. / Laschka, B. / ZShringer, C. et al. | British Library Conference Proceedings | 2001
      Publisher: AIAA
      Keywords: space planes , hypersonic systems , AIAA , hypersonic technologies

    Wind Tunnel Test Results for Gas Flows Inside Axisymmetric Cavities on Cylindric Bodies with Nose Cones

    Shvets, A. L. / Gilinsky, M. / Blankson, I. M. | NTRS | 2004
    Experimental test results of air flow inside and at the cylindrical cavity located on axisymmetric body are presented. These tests were ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Fluid Mechanics And Thermodynamics

    Wind Tunnel Results for Gas Flows Inside Axisymmetric Cavities on Cylindric Bodies with Nose Cones

    Shvets, Alexandr / Gilinsky, Mikhail / Blankson, Isaiah | AIAA | 2003
    Publisher: The American Institute of Aeronautics and Astronautics

    Weight Estimation of Hypersonic Waveriders Within the Integrated Design Program PrADO-Hy

    Bardenhagen, A. / Kossira, H. / Heinze, W. et al. | British Library Conference Proceedings | 1996
    Publisher: AIAA
    Keywords: space planes systems , hypersonic systems , AIAA , aerospace plane technologies

    Waverider Design and Analysis (AIAA 2015-3508)

    Ferguson, Frederick / Dhanasar, Mookesh / Blankson, Isaiah M. et al. | British Library Conference Proceedings | 2015
    Publisher: AIAA

    Waverider Design and Analysis

    Ferguson, Frederick / Dhanasar, Mookesh / Blankson, Isaiah M. | AIAA | 2015
    Publisher: The American Institute of Aeronautics and Astronautics

    Waverider Crossflow Model Validation for Radial and Length Variations Between Osculating Planes

    Clegg, Jon / Rodi, Patrick E. / Meade, Andrew | AIAA | 2020
    Publisher: The American Institute of Aeronautics and Astronautics

    Waverider Configuration Development for the Dual Fuel Vehicle

    Takashima, N. / Lewis, M. / Lockwood, M. et al. | British Library Conference Proceedings | 1996
    Publisher: AIAA
    Keywords: space planes systems , hypersonic systems , AIAA , aerospace plane technologies

    Waverider, A Revised Chronology (AIAA 2015-3529)

    Lunan, Duncan A. | British Library Conference Proceedings | 2015
    Publisher: AIAA

    Waverider, A Revised Chronology

    Lunan, Duncan A. | AIAA | 2015
    Publisher: The American Institute of Aeronautics and Astronautics

    Water Injection Pre-Compressor Cooling Assist Space Access

    Mehta, Unmeel / Bowles, Jeffrey / Melton, John et al. | AIAA | 2012
    Publisher: The American Institute of Aeronautics and Astronautics

      WATER INJECTION PRE-COMPRESSOR COOLING ASSIST SPACE ACCESS

      Mehta, U. / Bowles, J. / Melton, J. et al. | British Library Conference Proceedings | 2012
      Keywords: Space planes , Hypersonic systems

    Wall Pressure Effects and Shock-Boundary Layer Interactions in a Transpiration Cooled Scramjet Model Combustor

    Strauss, Friedolin T. / General, Stephan / Cragg, Patrick A. et al. | AIAA | 2020
    Publisher: The American Institute of Aeronautics and Astronautics

      WALL PRESSURE EFFECTS AND SHOCK-BOUNDARY LAYER INTERACTIONS IN A TRANSPIRATION COOLED SCRAMJET MODEL COMBUSTOR

      Strauss, Friedolin T. / Cragg, Stephan General. Patrick A. / Schlechtriem, Stefan | TIBKAT | 2020

    Wake Flow Control on the Afterburner behind Fuel Injection and Flame Holding Strut for Hypersonic Vehicle

    Araki, S. / Sakaue, S. / Arai, T. et al. | AIAA | 2012
    Publisher: The American Institute of Aeronautics and Astronautics

      WAKE FLOW CONTROL ON THE AFTERBURNER BEHIND FUEL INJECTION AND FLAME HOLDING STRUT FOR HYPERSONIC VEHICLE

      Araki, S. / Sakaue, S. / Arai, T. et al. | British Library Conference Proceedings | 2012
      Keywords: Space planes , Hypersonic systems

    VPSC, a vehicle parametric sizing code

    Hendrick, P. | AIAA | 2001
    Publisher: The American Institute of Aeronautics and Astronautics

    VORTICITY DISTRIBUTION IN LINEARIZED SUPERSONIC FLOW (AIAA 2018-5163)

    Gopal, Vijay / Maddalena, Luca | British Library Conference Proceedings | 2018
    Publisher: AIAA

    Vorticity Distribution in Linearized Supersonic Flow

    Gopal, Vijay / Maddalena, Luca | AIAA | 2018
    Publisher: The American Institute of Aeronautics and Astronautics

    Visualization of Unsteady Boundary-Layer Transition on Shock-Tube Wall using Highly Sensitive Fast-response TSP

    Ozawa, Hiroshi | AIAA | 2015
    Publisher: The American Institute of Aeronautics and Astronautics

    Visualization of Hypersonic Inward-Turning Inlet Flows by Planar Laser Scattering Method (AIAA 2017-2358)

    Li, Yiming / Li, Zhufei / Yang, Jiming et al. | British Library Conference Proceedings | 2017
    Publisher: AIAA

    Visualization of Hypersonic Inward-Turning Inlet Flows by Planar Laser Scattering Method

    Li, Yiming / Li, Zhufei / Yang, Jiming et al. | AIAA | 2017
    Publisher: The American Institute of Aeronautics and Astronautics

    Visualization of Hypersonic Boundary-Layer Transition on a Slender Cone (Invited) (AIAA 2014-3110)

    Laurence, S. / Wagner, A. / Ozawa, H. et al. | British Library Conference Proceedings | 2014
    Publisher: American Institute of Aeronautics and Astronautics , Reston, Va
    Keywords: Space planes , Hypersonic systems , AIAA

    Visualization of Hypersonic Boundary-Layer Transition on a Slender Cone (Invited)

    Laurence, Stuart J. / Wagner, Alexander / Ozawa, Hiroshi et al. | AIAA | 2014
    Publisher: The American Institute of Aeronautics and Astronautics

    Viscous Performance Map of a Blunt Streamline-Traced Busemann Inlet

    O'Brien, Timothy | AIAA | 2011
    Publisher: The American Institute of Aeronautics and Astronautics

      Viscous Performance Map of a Blunt Streamline-Traced Busemann Inlet

      O Brien, T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011
      Publisher: American Institute of Aeronautics and Astronautics , Reston, Va.
      Keywords: Space planes , Hypersonic systems , AIAA

    Viscous-Optimized Length-Constrained Axisymmetric Geometries for Streamline-Tracing

    O'Brien, Timothy | AIAA | 2008
    Publisher: The American Institute of Aeronautics and Astronautics

    Viscous-Optimized Length-Constrained Axisymmeric Geometries for Streamline-Tracing

    O Brien, T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008
    Publisher: AIAA , Reston
    Keywords: Space planes , Hypersonic systems

    Viscous drag reduction in a scramjet combustor with film cooling

    Rowan, S. / Paull, A. | AIAA | 2001
    Publisher: The American Institute of Aeronautics and Astronautics

    Viscous Drag Reduction in a Mach 12 Scramjet Engine

    Rowan, Scott / Takahashi, Masahiro / Sunami, Tetsuji et al. | AIAA | 2005
    Publisher: The American Institute of Aeronautics and Astronautics

    Virtual Experiment for Optimization of Fuel Distribution in a Scramjet Engine (AIAA 2015-3598)

    Sato, Shigeru / Fukui, Masaaki / Watanabe, Takahiro et al. | British Library Conference Proceedings | 2015
    Publisher: AIAA

    Virtual Experiment for Optimization of Fuel Distribution in a Scramjet Engine

    Sato, Shigeru / Fukui, Masaaki / Watanabe, Takahiro et al. | AIAA | 2015
    Publisher: The American Institute of Aeronautics and Astronautics

    Velocity Profile Modification in High-Speed Flows

    Barkmeyer, Daniel / Lewis, Mark | AIAA | 2003
    Publisher: The American Institute of Aeronautics and Astronautics

    Velocity measurement in a dual-mode supersonic combustor using particle image velocimetry

    Goyne, C. / McDaniel, J. / Krauss, R. et al. | AIAA | 2001
    Publisher: The American Institute of Aeronautics and Astronautics

    Velocity Field in Secondary Combustor of Ejector-Jet

    Nojima, Kiyoshi / Kouchi, Toshinori / Masuya, Goro et al. | AIAA | 2012
    Publisher: The American Institute of Aeronautics and Astronautics

      VELOCITY FIELD IN SECONDARY COMBUSTOR OF EJECTOR-JET

      Nojima, K. / Kouchi, T. / Masuya, G. et al. | British Library Conference Proceedings | 2012
      Keywords: Space planes , Hypersonic systems

    VeLChYD - Very Low Cost Hypersonic Demonstrator for a Complete Orbital Reentry Mission

    Chiesa, Sergio / Corpino, Sabrina / Plucinski, Krzysztof et al. | AIAA | 2005
    Publisher: The American Institute of Aeronautics and Astronautics

    Vehicle Systems

    Bowles, David | AIAA | 2003
    Publisher: The American Institute of Aeronautics and Astronautics

    Vehicle evaluations for tether-assisted launch to orbit

    Martin, J. / Hollowell, S. | AIAA | 2001
    Publisher: The American Institute of Aeronautics and Astronautics

    Vehicle concepts for an ejector ramjet combined cycle engine

    Lentsch, A. / Taguchi, H. / Shepperd, R. et al. | AIAA | 2001
    Publisher: The American Institute of Aeronautics and Astronautics