Subject: (34) Fluid Mechanics and Thermodynamics
Number of records: 44.
Iliff, Kenneth W. and Shafer, Mary F. (1995) A Comparison of Hypersonic Vehicle Flight and Prediction Results. Technical Report NASA TM-104313, Research Engineering, NASA Dryden Flight Research Center.
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.
Quinn, Robert D. and Gong, Leslie (2000) A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-Speed Aircraft. Technical Report NASA/TP-2000-209034, Research Engineering, NASA Dryden Flight Research Center.
Maine, Trindel A. and Gilyard, Glenn B. and Lambert, Heather H. (1990) A Preliminary Evaluation of an F100 Engine Parameter Estimation Process Using Flight Data. Technical Report NASA TM-4216, 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.
Gong, Leslie and Ko, William L. and Quinn, Robert D. and Richards, W. Lance (1987) Comparison of Flight-Measured and Calculated Temperatures on the Space Shuttle Orbiter. Technical Report NASA TM-88278, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Deaton, Vivian C. (1993) Correlation of Analytical and Experimental Hot Structure Vibration Results. Technical Report NASA TM-104269, Research Engineering, NASA Dryden Flight Research Center.
Greer, Donald (1999) Cryogenic Fuel Tank Draining Analysis Model. Meeting Paper CEC-ICMC CLB-3, Research Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. and Oates, David L. and Gonsalez, Jose C. (2000) Design and Evaluation of a New Boundary-Layer Rake for Flight Testing. Technical Report NASA/TM-2000-209014, Research Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. and Oates, David L. and Gonsalez, Jose C. (2000) Design and Evaluation of a New Boundary-Layer Rake for Flight Testing. Meeting Paper AIAA-2000-0503, Research Engineering, NASA Dryden Flight Research Center.
Noffz, Gregory K. and Bowman, Michael P. (1996) Design and Laboratory Validation of a Capacitive Sensor for Measuring the Recession of a Thin-Layered Ablator. Technical Report NASA TM-4777, Research Engineering, NASA Dryden Flight Research Center.
Sheridan, Arthur E. and Grier, Steven J. (1978) Drag Reduction Obtained by Modifying a Standard Truck. Technical Report NASA TM-72846, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Quinn, Robert D. and Gong, Leslie (1988) Effect of Internal Convection and Internal Radiation on the Structural Temperatures of Space Shuttle Orbiter. Technical Report NASA TM-100414, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Quinn, Robert D. and Gong, Leslie (1986) Effects of Forced and Free Convections on Structural Temperatures of Space Shuttle Orbiter During Reentry Flight. Technical Report NASA TM-86800 Revision, Research Engineering, NASA Dryden Flight Research Center.
Anderson, Bianca Trujillo and Meyer Jr., Robert R. (1990) Effects of Wing Sweep on Boundary-Layer Transition for a Smooth F-14A Wing at Mach Numbers From 0.700 To 0.825. Technical Report NASA TM-101712, Research Engineering, NASA Dryden Flight Research Center.
Anderson, Bianca Trujillo and Meyer Jr., Robert R. (1990) Effects of Wing Sweep on In-Flight Boundary-Layer Transition for a Laminar Flow Wing at Mach Numbers From 0.60 to 0.79. Technical Report NASA TM-101701, Research Engineering, NASA Dryden Flight Research Center.
Horn, Thomas J. and Abdelmessih, Amanie N. (2000) Experimental and Numerical Characterization of a Steady-State Cylindrical Blackbody Cavity at 1100 Degrees Celsius. Technical Report NASA/TM-2000-209022, Research Engineering, NASA Dryden Flight Research Center.
Horn, Thomas J. and Abdelmessih, Amanie N. (2000) Experimental and Numerical Characterization of a Steady-State Cylindrical Blackbody Cavity at 1100 Degrees Celsius. Meeting Paper ASME Paper NHTC2000-12140, Research Engineering, NASA Dryden Flight Research Center.
Noffz, Gregory K. and Lavine, Adrienne S. and Hamory, Philip J. (2003) Experimental Evaluation of Hot Films on Ceramic Substrates for Skin-Friction Measurement. Technical Report NASA/TM-2003-210742, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Quinn, Robert D. and Gong, Leslie (1986) Finite-Element Reentry Heat-Transfer Analysis of Space Shuttle Orbiter. Technical Report NASA TP-2657, Research Engineering, NASA Dryden Flight Research Center.
Powers, Sheryll Goecke and Huffman, Jarrett K. and Fox Jr., Charles H. (1986) Flight and Wind-Tunnel Measurements Showing Base Drag Reduction Provided by a Trailing Disk for High Reynolds Number Turbulent Flow for Subsonic and Transonic Mach Numbers. Technical Report NASA TP-2638, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Gong, Leslie and Quinn, Robert D. (2004) Hypothetical Reentry Thermostructural Performance of Space Shuttle Orbiter With Missing or Eroded Thermal Protection Tiles. Technical Report NASA/TM-2004-212850, Research Engineering, NASA Dryden Flight Research Center.
Quinn, Robert D. and Gong, Leslie (1980) In-Flight Boundary-Layer Measurements on a Hollow Cylinder at a Mach Number of 3.0. Technical Report NASA TP-1764, Research Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. and Pipitone, Brett J. and Krake, Keith L. (2003) In-Flight Capability for Evaluating Skin-Friction Gages and other Near-Wall Flow Sensors. Technical Report NASA/TM-2003-210738, Research Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. and Pipitone, Brett J. and Krake, Keith L. (2003) In-Flight Capability for Evaluating Skin-Friction Gages and Other Near-Wall Flow Sensors. Meeting Paper AIAA-2003-0741, Research Engineering, NASA Dryden Flight Research Center.
Wang, Kon-Sheng Charles (1994) In-Flight Imaging of Transverse Gas Jets Injected Into Transonic and Supersonic Crossflows: Design and Development. Technical Report NASA CR-186031, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Meyer Jr., Robert R. (1990) In-Flight Investigation of Shuttle Tile Pressure Orifice Installations. Technical Report NASA TM-4219, Research Engineering, NASA Dryden Flight Research Center.
Goecke Powers, Sheryll (1988) Influence of Base Modifications on In-Flight Base Drag in the Presence of Jet Exhaust for Mach Numbers From 0.7 to 1.5. Technical Report NASA TP-2802, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Tran, Van T. and Bowles, Jeff (2007) Lunar Return Reentry Thermal Analysis of a Generic Crew Exploration Vehicle Wall Structures. Technical Report NASA/TM-2007-214627, Research and Engineering, NASA Dryden Flight Research Center.
Banks, Daniel W. and Blanchard, Robert C. and Miller, Geoffrey M. (2004) Mobile Aerial Tracking and Imaging System (MATrIS) for Aeronautical Research. Technical Report NASA/TM-2004-212852, Research Engineering, NASA Dryden Flight Research Center.
Banks, D. W. and Blanchard, R. C. and Miller, G. M. (2004) Mobile Aerial Tracking and Imaging System (MATrIS) For Aeronautical Research. Meeting Paper ISFV106, Research Engineering, NASA Dryden Flight Research Center.
Greer, Donald S. (1994) Numerical Modeling of a Cryogenic Fluid Within a Fuel Tank. Technical Report NASA TM-4651, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Olona, Timothy and Muramoto, Kyle M. (1990) Optimum Element Density Studies for Finite-Element Thermal Analysis of Hypersonic Aircraft Structures. Technical Report NASA TM-4163, Research Engineering, NASA Dryden Flight Research Center.
Johnson, J. Blair (1988) Preliminary In-Flight Boundary Layer Transition Measurements on a 45-Degree Swept Wing at Mach Numbers Between 0.9 and 1.8. Technical Report NASA TM-100412, Research Engineering, NASA Dryden Flight Research Center.
Quinn, Robert D. and Gong, Leslie (1990) Real-Time Aerodynamic Heating and Surface Temperature Calculations for Hypersonic Flight Simulation. Technical Report NASA TM-4222, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Gong, Leslie and Quinn, Robert D. (2007) Reentry Thermal Analysis of a Generic Crew Exploration Vehicle Structure. Technical Report NASA/TM-2007-214607, 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 Engineering, NASA Dryden Flight Research Center.
Anderson, Bianca Trujillo and Meyer Jr., Robert R. and Chiles, Harry R. (1988) Techniques Used in the F-14 Variable-Sweep Transition Flight Experiment. Technical Report NASA TM-100444, 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.
Stephens, Craig A. and Hanna, Gregory J. (1991) Thermal Modeling and Analysis of a Cryogenic Tank Design Exposed to Extreme Heating Profiles. Technical Report NASA CR-186012, Research Engineering, NASA Dryden Flight Research Center.
Stephens, Craig A. and Hanna, Gregory J. and Gong, Leslie (1993) Thermal–Fluid Analysis of the Fill and Drain Operations of a Cryogenic Fuel Tank. Technical Report NASA TM-104273, Research Engineering, NASA Dryden Flight Research Center.
Banks, D. W. and van Dam, C. P. and Shiu, H. J. and Miller, G. M. (2000) Visualization of In-Flight Flow Phenomena Using Infrared Thermography. Technical Report NASA/TM-2000-209027, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. (1968) Wind-Tunnel Calibration of a 40 Degree Conical Pressure Probe at Mach Numbers from 3.5 to 7.4. Technical Report NASA Technical Note TN D-4678, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Fri Oct 10 18:15:38 PDT 2008.
