Subject: F-111
Number of records: 62.
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.
Jenkins, Jerald M. and Quinn, Robert D. (1996) A Historical Perspective of the YF-12A Thermal Loads and Structures Program. Technical Report NASA TM-104317, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Matheny, Neil W. and Kier, David A. and Manke, John A. (1968) A Preliminary Flying-Qualities Evaluation of a Variable-Sweep Fighter-Type Aircraft. Technical Report NASA TM X-1583, Research Engineering, NASA Dryden Flight Research Center.
Larson, Richard R. (1987) AFTI/F-111 MAW Flight Control System and Redundacy Management Description. Technical Report NASA TM-88267, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. (1971) An Investigation of Two Variations of the Gas Generator Method to Calculate the Thrust of the Afterburning Turbofan Engines Installed in an F-111A Airplane. Technical Report NASA Technical Note TN D-6297, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Hughes, Donald L. (1970) Analysis of In-Flight Pressure Fluctuations Leading to Engine Compressor Surge in an F-111A Airplane for Mach Numbers to 2.17, Conference Paper AIAA-1970-624, Research Engineering, NASA Flight Research Center.
Authors, Various (1980) Annual Report on Research and Technology Accomplishments. Technical Report NASA-TM-102949, Research Engineering, NASA Dryden Flight Research Center.
Redin, Paul C. (1981) Application of a Performance Modeling Technique to an Airplane with Variable Sweep Wings. Technical Report NASA TP-1855, Research Engineering, NASA Dryden Flight Research Center.
Bohn-Meyer, Marta R. (1988) Constructing "Gloved" Wings for Aerodynamic Studies. Technical Report NASA TM-100440, Research Engineering, NASA Dryden Flight Research Center.
Painter, Weneth D. and Caw, Lawrence J. (1979) Design and Physical Characteristics of the Transonic Aircraft Technology (TACT) Research Aircraft. Technical Report NASA TM-56048, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn (1996) Development of a Real-Time Transport Performance Optimization Methodology. Technical Report NASA TM-4730, Research Engineering, NASA Dryden Flight Research Center.
Moore, Archie L. and Harney, Constance D. (1988) Development of an Integrated Set of Research Facilities for the Support of Research Flight Test. Technical Report NASA TM-100427, Research Engineering, NASA Dryden Flight Research Center.
Moore, Archie L. and Harney, Constance D. (1988) Development of an Integrated Set of Research Facilities for the Support of Research Flight Test. Meeting Paper AIAA-1988-2096, Research Engineering, NASA Dryden Flight Research Center.
Comperini, Robert and Rhea, Donald C. (1988) Development of an Interactive Real-Time Graphics System for the Display of Vehicle Space Positioning. Technical Report NASA TM-100429, Research Engineering, NASA Dryden Flight Research Center.
Comperini, Robert and Rhea, Donald C. (1988) Development of an Interactive Real-Time Graphics System for the Display of Vehicle Space Positioning. Meeting Paper AIAA-1988-2167, 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.
Steers, Sandra Thornberry and Iliff, Kenneth W. (1975) Effects of Time-Shifted Data on Flight-Determined Stability and Control Derivatives. Technical Report NASA Technical Note TN D-7830, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L and Swann, Michael R. and Enevoldson, Einar K. and Wolf, Thomas D. (1983) Experience with Flight Test Trajectory Guidance. Journal of Guidance 6(5):393-398.
Swann, M.R. and Duke, E.L. and Enevoldson, E.K. and Wolf, T.D. (1981) Experience with Flight Test Trajectory Guidance. Meeting Paper AIAA-1981-2504, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Lawrence C. and Steers, Louis L. and Christopher, David and Trujillo, Bianca (1981) F-111 TACT Natural Laminar Flow Glove Flight Results. Conference Paper, NASA Conference Publication 2208, Research Engineering, NASA Dryden Flight Research Center.
Richardson, Robert B. and Harney, Paul F. (1968) Flight and Laboratory Testing of a Double Sideband FM Telemetry System. Technical Report NASA TM X-56015, 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.
Friend, Edward L. and Sakamoto, Glenn M. (1978) Flight Comparison of the Transonic Agility of the F-111A Airplane and the F-111 Supercritical Wing Airplane. Technical Report NASA TP-1368, Research Engineering, NASA Dryden Flight Research Center.
Larson, Richard R. (1986) Flight Control System Development and Flight Test Experience with the F-111 Mission Adaptive Wing Aircraft. Technical Report NASA TM-88265, Research Engineering, NASA Dryden Flight Research Center.
Larson, Richard R. (1986) Flight Control System Development and Flight Test Experience with the F-111 Mission Adaptive Wing Aircraft. Meeting Paper AIAA-1986-2237, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Batterton, Peter G. (1976) Flight Experience with a Digital Integrated Propulsion Control System on an F-111E Airplane. Meeting Paper AIAA-1976-653, Research Engineering, NASA Dryden Flight Research Center.
Powers, Sheryll Goecke (1988) Flight Tests of External Modifications Used to Reduce Blunt Base Drag. Technical Report NASA TM-100433, Research Engineering, NASA Dryden Flight Research Center.
Powers, Sheryll Goecke (1988) Flight Tests of External Modifications Used to Reduce Blunt Base Drag. Meeting Paper AIAA-1988-2553, Research Engineering, NASA Dryden Flight Research Center.
Powers, Sheryll Goecke and Webb, Lannie D. (1997) Flight Wing Surface Pressure and Boundary-Layer Data Report from the F-111 Smooth Variable-Camber Supercritical Mission Adaptive Wing. Technical Report NASA TM-4789, Research Engineering, NASA Dryden Flight Research Center.
Stewart, James F. and Burcham Jr., Frank W. and Gatlin, Donald H. (1992) Flight-Determined Benefits of Integrated Flight-Propulsion Control Systems. Technical Report NASA TM-4393, Research Engineering, NASA Dryden Flight Research Center.
Stewart, James F. and Burcham Jr., Frank W. and Gatlin, Donald H. (1992) Flight-Determined Benefits of Integrated Flight-Propulsion Control Systems. Meeting Paper ICAS 92-2.9.1, Research Engineering, NASA Dryden Flight Research Center.
Hughes, Donald L. and Holzman, Jon K. and Johnson, Harold J. (1972) Flight-Determined Characteristics of an Air Intake System on an F-111A Airplane. Technical Report NASA Technical Note TN D-6679, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex G. and Curry, Robert E. (1978) Flight-Determined Stability and Control Derivatives for the F-111 TACT Research Aircraft. Technical Report NASA Technical Paper TP-1350, Research Engineering, NASA Dryden Flight Research Center.
Monaghan, Richard C. (1978) Flight-Measured Buffet Characteristics of a Supercritical Wing and a Conventional Wing on a Variable-Sweep Airplane. Technical Report NASA TP-1244, Research Engineering, NASA Dryden Flight Research Center.
Nugent, Jack and Holzman, Jon K. (1974) Flight-Measured Inlet Pressure Transients Accompanying Engine Compressor Surges on The F-111A Airplane. Technical Report NASA Technical Note TN D-7696, Research Engineering, NASA Dryden Flight Research Center.
Taillon, Norman V. (1974) Flight-Test Investigation of the Aerodynamic Characteristics and Flow Interference Effects about the Aft Fuselage of the F-111A Airplane. Technical Report NASA Technical Note TN D-7563, Research Engineering, NASA Dryden Flight Research Center.
Bjarke, Lisa J. (1991) Flow Visualization Study of a 1/48-Scale AFTI/F111 Model to Investigate Horizontal Tail Flow Disturbances. Technical Report NASA TM-101698, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Meyer, Robert R. (1988) Flow Visualization Techniques for Flight Research. Technical Report NASA TM-100455, Research Engineering, NASA Dryden Flight Research Center.
Ayers, Theodore G. and Hallissy, James B. (1981) Historical Background and Design Evolution of the Transonic Aircraft Technology Supercritical Wing. Technical Report NASA TM-81356, Research Engineering, NASA Dryden Flight Research Center.
Meyer Jr., Robert R. and Jennett, Lisa A. (1985) In-Flight Surface Oil-Flow Photographs With Comparisons to Pressure Distribution and Boundary-Layer Data. Technical Report NASA TP-2395, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. (1973) Investigation of Coaxial Jet Noise and Inlet Choking Using an F-111A Airplane. Technical Report NASA Technical Note TN D-7376, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Lasagna, Paul L. and Oas, Stanley C. (1978) Measurements and Predictions of Flyover and Static Noise of a TF30 Afterburning Turbofan Engine. Technical Report NASA Technical Paper TP-1372, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. (1979) Measurements and Predictions of Flyover and Static Noise of an Afterburning Turbofan Engine in an F-111 Airplane. Meeting Paper AIAA-1979-7018, Research Engineering, NASA Dryden Flight Research Center.
Steers, Louis L. (1981) Natural Laminar Flow Flight Experiment. Conference Paper, NASA Conference Publication 2172, Research Engineering, NASA Dryden Flight Research Center.
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.
Smith, Ronald H. and Bellman, Donald R. and Hughes, Donald L. (1968) Preliminary Flight Investigation of Dynamic Phenomena Within Air Breathing Propulsion Systems of Supersonic Aircraft. Conference Paper AIAA-1968-593, Research Engineering, NASA Flight Research Center.
Hughes, Donald L. (1973) Pressures and Temperatures on the Lower Surfaces of an Externally Blown Flap System During Full-Scale Ground Tests. Technical Report NASA Technical Note TN D-7138, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Ray, Ronald J. and Conners, Timothy R. and Walsh, Kevin R. (1998) Propulsion Flight Research at NASA Dryden From 1967 to 1997. Technical Report NASA/TP-1998-206554, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Ray, Ronald J. and Conners, Timothy R. and Walsh, Kevin R. (1998) Propulsion Flight Research at NASA Dryden from 1967 to 1997. Meeting Paper AIAA-1998-3712, Research Engineering, NASA Dryden Flight Research Center.
Thornton, Stephen V. (1993) Reduction of Structural Loads Using Maneuver Load Control on the Advanced Fighter Technology Integration (AFTI)/F-111 Mission Adaptive Wing. Technical Report NASA TM-4526, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Ayers, Theodore G. (1995) Selected Examples of NACA/NASA Supersonic Flight Research. Technical Report NASA Special Publication SP-513, Research Engineering, NASA Dryden Flight Research Center. National Aeronautics and Space Administration.
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.
Burcham Jr., F.W. and Lasagna, P.L. and Kurtenbach, F.J. (1977) Static and Flyover Noise Measurements of an Inverted Profile Exhaust Jet. Meeting Paper ASME 77-GT-81, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Hughes, Donald L. and Holzman, Jon K. (1973) Steady-State and Dynamic Pressure Phenomena in the Propulsion System of an F-111A Airplane. Technical Report NASA Technical Note TN D-7328, Research Engineering, NASA Dryden Flight Research Center.
Nelson II, Sigurd A. (1994) Strain-Gage Selection in Loads Equations Using a Genetic Algorithm. Technical Report NASA CR-4597, Research Engineering, NASA Dryden Flight Research Center.
Bohn-Meyer, Marta and Jiran, Fred (1981) Techniques for Modifying Airfoils and Fairings on Aircraft Using Foam and Fiberglass. Conference Paper AIAA-1981-2445, Research Engineering, NASA Dryden Flight Research Center.
Bever, Glenn A. (1984) The Development of an Airborne Instrumentation Computer System for Flight Test. Technical Report NASA TM-86036, Research Engineering, NASA Dryden Flight Research Center.
Bellman, Donald R. and Hughes, Donald L. (1969) The Flight Investigation of Pressure Phenomena in the Air Intake of an F-111A Airplane. Conference Paper AIAA-1969-488, Research Engineering, NASA Flight Research Center.
Curry, Robert E. and Meyer Jr., Robert R. and O'Connor, Maureen (1984) The Use of Oil for In-Flight Flow Visualization. Technical Report NASA TM-84915, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. (1971) Use of the Gas Generator Method to Calculate the Thrust of an Afterburning Turbofan Engine. Meeting Paper AIAA-1971-680, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. (1978) Utilization of the Wing-Body Aerodynamic Analysis Program. Technical Report NASA TM-72856, Research Engineering, NASA Dryden Flight Research Center.
Smith, John W. and Lock, Wilton P. and Payne, Gordon A. (1992) Variable-Camber Systems Integration and Operational Performance of the AFTI/F-111 Mission Adaptive Wing. Technical Report NASA TM-4370, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sun Nov 22 18:16:17 PST 2009.
