Subject: HL-10
Number of records: 15.
Taylor Jr., Lawrence W. and Iliff, Kenneth W. and Powers, Bruce G. (1969) A Comparison of Newton-Raphson and Other Methods for Determining Stability Derivatives from Flight Data. Conference Paper AIAA-1969-315, Research Engineering, NASA Flight Research Center.
Saltzman, Edwin J. and Wang, K. Charles and Iliff, Kenneth W. (2002) Aerodynamic Assessment of Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations. Technical Report NASA/TP-2002-209032, Research Engineering, NASA Dryden Flight Research Center.
Banks, Daniel W. and Fisher, David F. (2006) Aft-End Flow of a Large-Scale Lifting Body During Free-Flight Tests. Technical Report NASA Meeting Presentation ISFV12, Research Engineering, NASA Dryden Flight Research Center.
Thompson, Milton O. and Weil, Joseph and Holleman, Euclid C. (1967) An Assessment of Lifting Reentry Flight Control Requirements During Abort, Terminal Glide, and Approach and Landing Situations. Technical Report NASA TM X-59119, Research Engineering, NASA Dryden Flight Research Center.
Kempel, Robert W. and Painter, Weneth D. and Thompson, Milton O. (1994) Developing and Flight Testing the HL-10 Lifting Body: A Precursor to the Space Shuttle. Technical Report NASA Reference Publication RP-1332, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. and Iliff, Kenneth W. and Whitman, Robert K. (1978) Effect of Sampling Rate and Record Length on the Determination of Stability and Control Derivatives. Technical Report NASA TM-72858, Research Engineering, NASA Dryden Flight Research Center.
Kempel, Robert W. and Manke, John A. (1974) Flight Evaluation of HL-10 Lifting Body Handling Qualities at Mach Numbers from 0.30 to 1.86. Technical Report NASA Technical Note TN D-7537, Research Engineering, NASA Dryden Flight Research Center.
Tang, Ming H. and Pearson, George P. E. (1971) Flight-Measured HL-10 Lifting Body Center Fin Loads and Control Surface Hinge Moments and Correlation With Wind-Tunnel Predictions. Technical Report NASA TM X-2419, Research Engineering, NASA Dryden Flight Research Center.
Painter, Weneth D. and Sitterle, George J. (1974) HL-10 Lifting Body Flight Control System Characteristics and Operational Experience. Technical Report NASA TM X-2956, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Wang, K. Charles and Iliff, Kenneth W. (2007) In-Flight Subsonic Lift and Drag Characteristics Unique to Blunt-Based Lifting Reentry Vehicles. Journal Article AIAA-18365, Research and Engineering, NASA Dryden Flight Research Center. Journal of Spacecraft and Rockets 44(2):299-309.
Walker, Harold J. (1979) Performance Evaluation Method for Dissimilar Aircraft Designs. Technical Report NASA Reference Publication RP-1042, Research Engineering, NASA Dryden Flight Research Center.
Jones, Daniel S. and Ray, Ronald J. and Phillips, Paul (2005) Rehabilitation of the Rocket Vehicle Integration Test Stand at Edwards Air Force Base. Technical Report NASA/TM-2005-212863, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex G. (1973) Results of a Feasibility Study Using the Newton-Raphson Digital Computer Program to Identify Lifting Body Derivatives from Flight Data. Technical Report NASA TM X-56017, 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.
Larson, Richard R. (1972) Statistical Analysis of Landing Contact Conditions for Three Lifting Body Research Vehicles. Technical Report NASA Technical Note TN D-6708, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Fri Oct 10 18:16:36 PDT 2008.
