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Subject: B-52


Number of records: 17.

Pak, Chan-gi (2008) Aeroservoelastic Stability Analysis of the X-43A Stack. Technical Report NASA/TM-2008-214635, Research and Engineering, NASA Dryden Flight Research Center.

Ko, William L. (2003) Aging Theories for Establishing Safe Life Spans of Airborne Critical Structural Components. Technical Report NASA/TP-2003-212034, Research Engineering, NASA Dryden Flight Research Center.

Ko, W.L. and Carter, A.L. and Totton, W.W. and Ficke, J.M. (1989) Application of Fracture Mechanics and Half-Cycle Method to the Prediction of Fatigue Life of B-52 Aircraft Pylon Components. Technical Report NASA TM-88277, Research Engineering, NASA Dryden Flight Research Center.

Whitmore, Stephen A. and Cobleigh, Brent R. and Jacobson, Steven R. and Jensen, Steven C. and Hennings, Elsa J. (2004) Development and Testing of a Drogue Parachute System for X-37 ALTV/B-52H Separation. Technical Report NASA/TM-2004-212044, Research Engineering, NASA Dryden Flight Research Center.

Whitmore, Stephen A. and Cobleigh, Brent R. and Jacobson, Steven R. and Jensen, Steven C. and Hennings, Elsa J. (2004) Development and Testing of a Drogue Parachute System For X-37 ALTV/B-52H Separation. Meeting Paper AIAA-2004-873, Research Engineering, NASA Dryden Flight Research Center.

Andrews, William H. and Robinson, Glenn H. and Larson, Richard R. (1972) Exploratory Flight Investigation of Aircraft Response to The Wing Vortex Wake Generated by Jet Transport Aircraft. Technical Report NASA Technical Note TN D-6655, Research Engineering, NASA Dryden Flight Research Center.

Ko, William L. and Chen, Tony (2006) Extended Aging Theories for Predictions of Safe Operational Life of Critical Airborne Structural Components. Technical Report NASA/TP-2006-213676, 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.

Ko, William L. and Schuster, Lawrence S. (1984) Preflight Transient Dynamic Analyses of B-52 Aircraft Carrying Space Shuttle Solid Rocket Booster Drop-Test Vehicle. Technical Report NASA TM-84925, Research Engineering, NASA Dryden Flight Research Center.

Ko, William L. and Schuster, Lawrence S. (1983) Preflight Transient Dynamic Analyses of B-52 Aircraft Carrying Space Shuttle Solid Rocket Booster Drop-Test Vehicle. Meeting Paper AIAA-1983-2698, 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. and Schuster, Lawrence S. (1985) Stress Analyses of B-52 Pylon Hooks. Technical Report NASA TM-84924, Research Engineering, NASA Dryden Flight Research Center.

Ko, William L. (1997) Stress Analysis of B-52 Pylon Hooks for Carrying the X-38 Drop Test Vehicle. Technical Report NASA/TM-97-206218, Research 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.

Holleman, Euclid C. (1976) Summary of Flight Tests to Determine the Spin and Controllability Characteristics of a Remotely Piloted, Large-Scale (3/8) Fighter Airplane Model. Technical Report NASA Technical Note TN D-8052, Research Engineering, NASA Dryden Flight Research Center.

Davis, Mark C. and Sim, Alexander G. and Rhode, Matthew and Johnson, Kevin D. (2006) Wind Tunnel Results of the B-52B with the X-43A Stack. Conference Paper AIAA-2006-3850.

Vachon, Michael Jacob and Grindle, Thomas J. and St. John, Clinton W. and Dowdell, David B. (2005) X-43A Fluid and Environmental Systems: Ground and Flight Operation and Lessons Learned. Conference Presentation AIAA-2005-3337, Research Engineering, NASA Dryden Flight Research Center.

This list was generated on Sun Nov 22 18:16:04 PST 2009.

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Last Modified: September 14, 2004
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