Subject: Pegasus

• Subject Areas (1620)
  • Aircraft/Project (1292)
    • Pegasus (22)

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Number of records: 22.

Fricker, Darren and Mendoza, John and Catton, Ivan (1992) A Computational Fluid Dynamics Analysis of the Hypersonic Flights of Pegasus®. Technical Report NASA CR-186023, Research Engineering, NASA Dryden Flight Research Center.

Bertelrud, Arild and Budd, Jerry and Sollberger, David and Churchward, Rex and Smilg, Larry and Stowers, Jim (1999) A Hypersonic Flight Test to Document Laminar/Turbulent Transition. Meeting Paper AIAA-1999-4849, Research Engineering, NASA Dryden Flight Research Center.

Mendenhall, Michael R. and Lesieutre, Daniel J. and Whittaker, C. Helen and Curry, Robert E. and Moulton, Bryan (1993) Aerodynamic Analysis of Pegasus™ - Computations vs Reality. Meeting Paper AIAA-1993-0520, Research Engineering, NASA Dryden Flight Research Center.

Mendenhall, M.R. and Hegedus, M.C. and Budd, G.D. and Frackowiak, A.J. (1997) Aerodynamic Analysis of the Deep-Stall Flight Characteristics of the Pegasus XL Booster. Meeting Paper AIAA-1997-3583, Research Engineering, NASA Dryden Flight Research Center.

Meyer Jr., Robert R. and Curry, Robert E. and Budd, Gerald D. (1992) Aerodynamic Flight Research Using the Pegasus® Air-Launched Space Booster. Meeting Paper AIAA-1992-3990, Research Engineering, NASA Dryden Flight Research Center.

Noffz, Gregory K. and Curry, Robert E. and Haering Jr., Edward A. and Kolodziej, Paul (1991) Aerothermal Test Results From the First Flight of the Pegasus Air-Launched Space Booster. Technical Report NASA TM-4330, Research Engineering, NASA Dryden Flight Research Center.

Noffz, Gregory K. and Moes, Timothy R. and Haering Jr., Edward A. and Kolodziej, Paul (1992) Aerothermal Test Results From the Second Flight of the Pegasus® Booster. Technical Report NASA TM-4391, Research Engineering, NASA Dryden Flight Research Center.

Richards, W. Lance and Monaghan, Richard C. (1996) Analytical and Experimental Verification of a Flight Article for a Mach-8 Boundary-Layer Experiment. Technical Report NASA TM-4733, Research Engineering, NASA Dryden Flight Research Center.

Richards, W. Lance (1997) Finite-Element Analysis of a Mach-8 Flight Test Article Using Nonlinear Contact Elements. Technical Report NASA TM-4796, Research Engineering, NASA Dryden Flight Research Center.

Curry, Robert E. and Mendenhall, Michael R. and Moulton, Bryan (1992) In-Flight Evaluation of Aerodynamic Predictions of an Air-Launched Space Booster. Technical Report NASA TM-104246, Research Engineering, NASA Dryden Flight Research Center.

Ko, William L. and Tran, Van T. and Chen, Tony (2007) Incorporation of Half-Cycle Theory Into Ko Aging Theory for Aerostructural Flight-Life Predictions. Technical Report NASA/TP-2007-214608, Research and Engineering, NASA Dryden Flight Research Center.

Meyer, Robert R. (1992) Overview of the NASA Dryden Flight Research Facility Aeronautical Flight Projects. Technical Report NASA TM-104254, Research Engineering, NASA Dryden Flight Research Center.

Bertelrud, A. and de la Tova, G. and Budd, G.B. and Noffz, G. and Richards, W.L. and Monaghan, R.C. (1998) Pegasus® Wing-Glove Experiment to Document Crossflow Transition-Development and Current Status. Meeting Paper AIAA-1998-1522, Research Engineering, NASA Dryden Flight Research Center.

Bertelrud, Arild and de la Tova, Geva and Hamory, Philip J. and Young, Ronald and Noffz, Gregory K. and Dodson, Michael and Graves, Sharon S. and Diamond, John K. and Bartlett, James E. and Noack, Robert and Knoblock, David (2000) Pegasus® Wing-Glove Experiment to Document Hypersonic Crossflow Transition-Measurement System and Selected Flight Results. Meeting Paper AIAA-2000-0505, Research Engineering, NASA Dryden Flight Research Center.

Bertelrud, Arild and de la Tova, Geva and Hamory, Philip J. and Young, Ronald and Noffz, Gregory K. and Dodson, Michael and Graves, Sharon S. and Diamond, John K. and Bartlett, James E. and Noack, Robert and Knoblock, David (2000) Pegasus® Wing-Glove Experiment to Document Hypersonic Crossflow Transition—Measurement System and Selected Flight Results. Technical Report NASA/TM-2000-209016, Research Engineering, NASA Dryden Flight Research Center.

Bertelrud, Arild and Kolodziej, Paul and Noffz, Greg K. and Godil, Afzal (1992) Plans for In-Flight Measurement of Hypersonic Crossflow Transition on the Pegasus® Launch Vehicle. Meeting Paper AIAA-1992-4104, Research Engineering, NASA Dryden Flight Research Center.

Gong, Leslie and Richards, W. Lance and Monaghan, Richard C. and Quinn, Robert D. (1993) Preliminary Analysis for a Mach 8 Crossflow Transition Experiment on the Pegasus® Space Booster. Technical Report NASA TM-104272, Research Engineering, NASA Dryden Flight Research Center.

Fisher, David F. (2007) Six Decades of Flight Research: An Annotated Bibliography of Technical Publications of NASA Dryden Flight Research Center, 1946-2006. Technical Report NASA/TP-2007-213684, Research and Engineering, NASA Dryden Flight Research Center.

Ko, William L. (2005) Stress Analysis of B-52B and B-52H Air-Launching Systems Failure-Critical Structural Components. Technical Report NASA/TP-2005-212862, Research Engineering, NASA Dryden Flight Research Center.

Gong, Leslie and Richards, W. Lance (1998) Thermal Analysis of a Metallic Wing Glove for a Mach-8 Boundary-Layer Experiment. Technical Report NASA/TM-1998-206555, Research Engineering, NASA Dryden Flight Research Center.

Gong, Leslie and Richards, W. Lance (1998) Thermal Analysis of a Metallic Wing Glove for a Mach-8 Boundary-Layer Experiment. Meeting Paper AIAA-1998-2580, Research Engineering, NASA Dryden Flight Research Center.

Ko, William L. and Gong, Leslie (2000) Thermoelastic Analysis of Hyper-X Camera Windows Suddenly Exposed to Mach 7 Stagnation Aerothermal Shock. Technical Report NASA/TP-2000-209030, Research Engineering, NASA Dryden Flight Research Center.

This list was generated on Sun Nov 22 18:17:00 PST 2009.