Subject: F-16XL
Number of records: 23.
Kehoe, Michael W. (1995) A Historical Overview of Flight Flutter Testing. Technical Report NASA TM-4720, Research Engineering, NASA Dryden Flight Research Center.
Olney, Candida D. and Collura, Joseph V. (1997) A Limited In-Flight Evaluation of the Constant Current Loop Strain Measurement Method. Technical Report NASA TM-104331, Research Engineering, NASA Dryden Flight Research Center.
Flores, Jolen and Tu, Eugene and Anderson, Bianca and Landers, Stephen (1991) A Parametric Study of the Leading Edge Attachment Line for the F-16XL. Meeting Paper AIAA-1991-1621, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Haering Jr., Edward A. and Ehernberger, L.J. (1996) An Optimal Deconvolution Method for Reconstructing Pneumatically Distorted Near-Field Sonic Boom Pressure Measurement. NASA Technical Paper 4000, Research and Engineering, NASA Dryden Flight Research Center.
Smith, John W. and Montgomery, Terry (1996) Biomechanically Induced and Controller Coupled Oscillations Experienced on the F-16XL Aircraft During Rolling Maneuvers. Technical Report NASA TM-4752, Research Engineering, NASA Dryden Flight Research Center.
Marshall, Laurie A. (1999) Boundary-Layer Transition Results From the F-16XL-2 Supersonic Laminar Flow Control Experiment. Technical Report NASA/TM-1999-209013, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. (1997) Dynamic Ground Effect for a Cranked Arrow Wing Airplane. Technical Report NASA TM-4799, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. (1997) Dynamic Ground Effect for a Cranked Arrow Wing Airplane. Meeting Paper AIAA-1997-3649 Research Engineering, NASA Dryden Flight Research Center.
Ennix, Kimberly A. (1993) Engine Exhaust Characteristics Evaluation in Support of Acoustic Testing. Technical Report NASA TM-104263, Research Engineering, NASA Dryden Flight Research Center.
Landers, Stephen F. and Saltzman, John A. and Bjarke, Lisa J. (1997) F-16XL Wing Pressure Distributions and Shock Fence Results from Mach 1.4 to Mach 2.0. Technical Report NASA/TM-97-206219, Research Engineering, NASA Dryden Flight Research Center.
Holzman, Jon K. and Webb, Lannie D. and Burcham Jr., Frank W. (1996) Flight and Static Exhaust Flow Properties of an F110-GE-129 Engine in an F-16XL Airplane During Acoustic Tests. Technical Report NASA TM-104326, Research Engineering, NASA Dryden Flight Research Center.
Stachowiak, Susan J. and Bosworth, John T. (2004) Flight Test Results for the F-16XL With a Digital Flight Control System. Technical Report NASA/TP-2004-212046, Research Engineering, NASA Dryden Flight Research Center.
Voracek, David F. (1993) Ground Vibration and Flight Flutter Tests of the Single-Seat F-16XL Aircraft With a Modified Wing. Technical Report NASA TM-104264, Research Engineering, NASA Dryden Flight Research Center.
Vernon, Lura (1993) In-flight Investigation of a Rotating Cylinder-Based Structural Excitation System for Flutter Testing. Technical Report NASA TM-4512, Research Engineering, NASA Dryden Flight Research Center.
Vernon, Lura (1993) In-Flight Investigation of a Rotating Cylinder-Based Structural Excitation System for Flutter Testing. Meeting Paper AIAA-1993-1537, Research Engineering, NASA Dryden Flight Research Center.
Anderson, Bianca T. and Bohn-Meyer, Marta (1992) Overview of Supersonic Laminar Flow Control Research on the F-16XL Ships 1 and 2. Technical Report NASA TM-104257, Research Engineering, NASA Dryden Flight Research Center.
Anderson, Bianca T. and Bohn-Meyer, Marta (1992) Overview of Supersonic Laminar Flow Control Research on the F-16XL Ships 1 and 2. Meeting Paper SAE Paper 921994, Research 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.
Schneider, Edward T. (1990) Piloted Simulator Assessments of Agility. Meeting Paper AIAA-1990-1306, Research Engineering, NASA Dryden Flight Research Center.
Haering Jr., Edward A. and Ehernberger, L. J. and Whitmore, Stephen A. (1995) Preliminary Airborne Measurements for the SR-71 Sonic Boom Propagation Experiment. Technical Report NASA TM-104307, Research Engineering, NASA Dryden Flight Research Center.
Haering Jr., Edward A. and Ehernberger, L.J. and Whitmore, Stephen A. (1996) Preliminary Airborne Measurements for the SR-71 Sonic Boom Propagation Experiment. In Proceedings 1995 NASA High-Speed Research Program Sonic Boom Workshop I, pages 176-198, Langley Research Center, Hampton, Virginia.
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.
Marshall, Laurie A. (2000) Summary of Transition Results from the F-16XL-2 Supersonic Laminar Flow Control Experiment. Meeting Paper AIAA-2000-4418, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sun Nov 22 18:16:26 PST 2009.
