Subject: X-29
Number of records: 94.
Bosworth, John T. and Cox, Timothy H. (1989) A Design Procedure for the Handling Qualities Optimization of the X-29A Aircraft. Technical Report NASA TM-4142, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. and Cox, Timothy H. (1989) A Design Procedure for the Handling Qualities Optimization of the X-29A Aircraft. Meeting Paper AIAA-1989-3428, Research Engineering, NASA Dryden Flight Research Center.
Mackall, Dale A. and Allen, James G. (1989) A Knowledge-Based System Design/Information Tool for Aircraft Flight Control Systems. Technical Report NASA TM-101704, Research Engineering, NASA Dryden Flight Research Center.
Mackall, Dale A. and Allen, James G. (1989) A Knowledge-Based System Design/Information Tool for Aircraft Flight Control Systems. Meeting Paper AIAA-1989-2978, Research Engineering, NASA Dryden Flight Research Center.
Stewart, James F. and Bauer, Carol A. (1983) A Project Management System for the X-29A Flight Test Program. Meeting Paper AIAA-1983-2712, Research Engineering, NASA Dryden Flight Research Center.
Bjarke, Lisa J. and Del Frate, John H. and Fisher, David F. (1992) A Summary of the Forebody High-Angle-of-Attack Aerodynamics Research on the F-18 and the X-29A Aircraft. Technical Report NASA TM-104261, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. (1987) Aircraft Ground Vibration Testing at NASA Ames-Dryden Flight Research Facility. Technical Report NASA TM-88272, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Laurie, Edward J. and Bjarke, Lisa J. (1990) An In-Flight Interaction of the X-29A Canard and Flight Control System. Technical Report NASA TM-101718, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Laurie, Edward J. and Bjarke, Lisa J. (1990) An In-Flight Interaction of the X-29A Canard and Flight Control System. Meeting Paper AIAA-1990-1240, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. and Moulton, Bryan J. and Kresse, John (1989) An In-Flight Investigation of Ground Effect on a Forward-Swept Wing Airplane. Technical Report NASA TM-101708, Research Engineering, NASA Dryden Flight Research Center.
Glover, Richard D. (1983) Application Experience with the NASA Aircraft Interrogation and Display System: A Ground Support Equipment for Digital Flight Systems.
Sarrafian, Shahan K. and Powers, Bruce G. (1985) Application of Frequency Domain Handling Qualities Criteria to the Longitudinal Landing Task. Meeting Paper AIAA-1985-1848, Research Engineering, NASA Dryden Flight Research Center.
Maine, Richard E. and Murray, James E. (1986) Application of Parameter Estimation to Highly Unstable Aircraft. Technical Report NASA TM-88266, Research Engineering, NASA Dryden Flight Research Center.
Maine, Richard E. and Murray, James E. (1986) Application of Parameter Estimation to Highly Unstable Aircraft. Meeting Paper AIAA-1986-2020, Research Engineering, NASA Dryden Flight Research Center.
Voracek, David F. and Clarke, Robert (1991) Buffet Induced Structural/Flight-Control System Interaction of the X-29A Arcraft. Technical Report NASA TM-101735, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Kania, Jan and Pearce, Robert and Mills, Glen (1987) Challenges in Modeling the X-29 Flight Test Performance. Technical Report NASA TM-88282, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Kania, Jan and Pearce, Robert and Mills, Glen (1987) Challenges in Modeling the X-29A Flight Test Performance. Meeting Paper AIAA-1987-0081, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Richwine, David M. and Landers, Stephen (1992) Correlation of Forebody Pressures and Aircraft Yawing Moments on the X-29A Aircraft at High Angles of Attack. Technical Report NASA TM-4417, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Richwine, David M. and Landers, Stephen (1992) Correlation of Forebody Pressures and Aircraft Yawing Moments on the X-29A Aircraft at High Angles of Attack. Meeting Paper AIAA-1992-4105, Research Engineering, NASA Dryden Flight Research Center.
Schuster, Lawrence S. and Lokos, William A. (1988) Current Flight Test Experience Related to Structural Divergence of Forward-Swept Wings. Technical Report NASA TM-100445, Research Engineering, NASA Dryden Flight Research Center.
Glover, Richard D. (1987) Design and Initial Application of the Extended Aircraft Interrogation and Display System - Multiprocessing Ground Support Equipment for Digital Flight Systems. Technical Report NASA TM-86740, Research Engineering, NASA Dryden Flight Research Center.
Knighton, Donna L. (1992) Design and Utilization of a Flight Test Engineering Database Management System at the NASA Dryden Flight Research Facility. Meeting Paper AIAA-1992-4072, Research Engineering, NASA Dryden Flight Research Center.
Ray, R.J. and Hicks, J.W. and Alexander, R.I. (1988) Development of a Real-Time Aeroperformance Analysis Technique for the X-29A Advanced Technology Demonstrator. Technical Report NASA TM-100432, Research Engineering, NASA Dryden Flight Research Center.
Ray, R.J. and Hicks, J.W. and Alexander, R.I. (1988) Development of a Real-Time Aeroperformance Analysis Technique for the X-29A Advanced Technology Demonstrator. Meeting Paper AIAA-1988-2145, Research Engineering, NASA Dryden Flight Research Center.
Gupta, K.K. and Brenner, M.J. and Voelker, L.S. (1991) Development of an Integrated Aeroservoelastic Analysis Program and Correlation With Test Data. Technical Report NASA Technical Paper TP-3120, 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.
Gera, Joseph and Bosworth, John T. (1987) Dynamic Stability and Handling Qualities Tests on a Highly Augmented, Statically Unstable Airplane. Meeting Paper AIAA-1987-2258, Research Engineering, NASA Dryden Flight Research Center.
Gera, Joseph (1986) Dynamics and Controls Flight Testing of the X-29A Airplane. Technical Report NASA TM-86803, Research Engineering, NASA Dryden Flight Research Center.
Gera, Joseph (1986) Dynamics and Controls Flight Testing of the X-29A Airplane. Meeting Paper AIAA-1986-0167, Research Engineering, NASA Dryden Flight Research Center.
Smith, Rogers E. and Sarrafian, Shahan K. (1986) Effect of Time Delay on Flying Qualities: An Update. Technical Report NASA TM-88264, Research Engineering, NASA Dryden Flight Research Center.
Smith, Rogers E. and Sarrafian, Shahan K. (1986) Effect of Time Delay on Flying Qualities: An Update. Meeting Paper AIAA-1986-2202, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Moulton, Bryan J. (1988) Effects of Maneuver Dynamics on Drag Polars of the X-29A Forward-Swept-Wing Aircraft with Automatic Wing Camber Control. Meeting Paper AIAA-1988-2144, Research Engineering, NASA Dryden Flight Research Center.
Bauer, Jeffrey E. and Andrisani, Dominick (1990) Estimating Short-Period Dynamics Using an Extended Kalman Filter. Technical Report NASA TM-101722, Research Engineering, NASA Dryden Flight Research Center.
Ray, Ronald J. (1994) Evaluating the Dynamic Response of In-Flight Thrust Calculation Techniques During Throttle Transients. Technical Report NASA TM-4591, Research Engineering, NASA Dryden Flight Research Center.
Ray, Ronald J. (1990) Evaluation of Various Thrust Calibration Techniques on an F404 Engine. Technical Report NASA TP-3001, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Regenie, Victoria A. (1985) Expert Systems Development and Application. Technical Report NASA TM-86746, Research Engineering, NASA Dryden Flight Research Center.
Sitz, Joel R. and Vernon, Todd H. (1990) Flight Control System Design Factors for Applying Automated Testing Techniques. Technical Report NASA TM-4242, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. and Ayers, Theodore G. (1988) Flight Research and Testing. Technical Report NASA TM-100439, Research Engineering, NASA Dryden Flight Research Center.
Bauer, Jeffrey E. and Clarke, Robert and Burken, John J. (1995) Flight Test of the X-29A at High Angle of Attack: Flight Dynamics and Controls. Technical Report NASA TP-3537, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Cooper Jr., James M. and Sefic, Walter J. (1987) Flight Test Techniques for the X-29A Aircraft. Technical Report NASA TM-88289, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Cooper Jr., James M. and Sefic, Walter J. (1987) Flight Test Techniques for the X-29A Aircraft. Meeting Paper AIAA-1987-0082, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. (1992) Flight-Determined Stability Analysis of Multiple-Input-Multiple-Output Control Systems. Meeting Paper AIAA-1992-4396, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. (1992) Flight-Determined Stability Analysis of Multiple-Input–Multiple-Output Control Systems. Technical Report NASA TM-4416, 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.
Cotton, Lt. Stacey J. and Bjarke, Lisa J. (1994) Flow-Visualization Study of the X-29A Aircraft at High Angles of Attack Using a 1/48-Scale Model. Technical Report NASA TM-104268, Research Engineering, NASA Dryden Flight Research Center.
Del Frate, John H. and Saltzman, John A. (1992) In-Flight Flow Visualization Results From the X-29A Aircraft at High Angles of Attack. Technical Report NASA TM-4430, Research Engineering, NASA Dryden Flight Research Center.
Del Frate, John H. and Saltzman, John A. (1992) In-Flight Flow Visualization Results from the X-29A Aircraft at High Angles of Attack. Meeting Paper AIAA-1992-4102, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Hicks, John W. (1994) In-Flight Lift-Drag Characteristics for a Forward-Swept-Wing Aircraft (and Comparisons With Contemporary Aircraft). Technical Report NASA TP-3414, Research Engineering, NASA Dryden Flight Research Center.
Shafer, Mary F. (1992) In-Flight Simulation Studies at the NASA Dryden Flight Research Facility. Technical Report NASA TM-4396, Research Engineering, NASA Dryden Flight Research Center.
Earls, Michael R. and Sitz, Joel R. (1989) Initial Flight Qualification and Operational Maintenance of X-29A Flight Software. Technical Report NASA TM-101703, Research Engineering, NASA Dryden Flight Research Center.
Earls, Michael R. and Sitz, Joel R. (1989) Initial Flight Qualification and Operational Maintenance of X-29A Flight Software. Meeting Paper AIAA-1989-3596, Research Engineering, NASA Dryden Flight Research Center.
Shafer, Mary F. and Koehler, Ruthard and Wilson, Edward M. and Levy, David R. (1989) Initial Flight Test of a Ground Deployed System for Flying Qualities Assessment. Technical Report NASA TM-101700, Research Engineering, NASA Dryden Flight Research Center.
Shafer, Mary F. and Koehler, Ruthard and Wilson, Edward M. and Levy, David R. (1989) Initial Flight Test of a Ground Deployed System for Flying Qualities Assessment. Meeting Paper AIAA-1989-3359, Research Engineering, NASA Dryden Flight Research Center.
Gupta, K.K. and Brenner, M.J. and Voelker, L.S. (1987) Integrated Aeroservoelastic Analysis Capability with X-29A Analytical Comparisons. Meeting Paper AIAA-1987-0907, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. (1992) Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison With Flight Data. Technical Report NASA TM-4356, Research Engineering, NASA Dryden Flight Research Center.
Conners, Timothy R. (1989) Measurement Effects on the Calculation of In-Flight Thrust for an F404 Turbofan Engine. Technical Report NASA TM-4140, Research Engineering, NASA Dryden Flight Research Center.
Conners, Timothy R. (1989) Measurement Effects on the Calculation of In-Flight Thrust for an F404 Turbofan Engine. Meeting Paper AIAA-1989-2364, Research Engineering, NASA Dryden Flight Research Center.
Voracek, David F. (1990) Monitoring Techniques for the X-29A Aircraft's High-Speed Rotating Power Takeoff Shaft. Technical Report NASA TM-101731, Research Engineering, NASA Dryden Flight Research Center.
Chacon, Vince and McBride, David (1988) Operational Viewpoint of the X-29A Digital Flight Control System. Technical Report NASA TM-100434, Research Engineering, NASA Dryden Flight Research Center.
Mackall, Dale and McBride, David and Cohen, Dorothea (1990) Overview of the NASA Ames-Dryden Integrated Test Facility. Technical Report NASA TM-101720, 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.
Budd, Gerald D. (1987) Predicted Pitching Moment Characteristics of X-29A Aircraft. Technical Report NASA TM-88284, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Matheny, Neil W. (1987) Preliminary Flight Assessment of the X-29A Advanced Technology Demonstrator. Technical Report NASA TM-100407, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Matheny, Neil W. (1987) Preliminary Flight Assessment of the X-29A Advanced Technology Demonstrator. Meeting Paper AIAA-1987-2949, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Huckabone, Thomas (1989) Preliminary Flight-Determined Subsonic Lift and Drag Characteristics of the X-29A Forward-Swept-Wing Airplane. Technical Report NASA TM-100409, Research Engineering, NASA Dryden Flight Research Center.
Stewart, James F. and Bauer, Carol A. (1983) Project Management Techniques for Highly Integrated Programs. Technical Report NASA TM-86023, Research Engineering, NASA Dryden Flight Research Center.
Mackall, Dale A. (1985) Qualification Needs for Advanced Integrated Aircraft. Technical Report NASA TM-86731, Research Engineering, NASA Dryden Flight Research Center.
Davis, Steven B. (1990) Real-Time Application of Advanced Three-Dimensional Graphic Techniques for Research Aircraft Simulation. Technical Report NASA TM-101730, Research Engineering, NASA Dryden Flight Research Center.
Bauer, Jeffrey E. and Crawford, David B. and Gera, Joseph and Andrisani II, Dominick (1987) Real-Time Comparison of X-29A Flight Data and Simulation Data. Meeting Paper AIAA-1987-0344, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Petersen, Kevin L. (1988) Real-Time Flight Test Analysis and Display Techniques for the X-29A Aircraft. Technical Report NASA TM-101692, Research Engineering, NASA Dryden Flight Research Center.
Ray, Ronald J. and Hicks, John W. and Wichman, Keith D. (1991) Real-Time In-Flight Engine Performance and Health Monitoring Techniques for Flight Research Application. Technical Report NASA TM-104239, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Cobleigh, Brent R. and Banks, Daniel W. and Hall, Robert M. and Wahls, Richard W. (1998) Reynolds Number Effects at High Angles of Attack. Technical Report NASA/TP-1998-206553, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Cobleigh, Brent R. and Banks, Daniel W. and Hall, Robert M. and Wahls, Richard A. (1998) Reynolds Number Effects at High Angles of Attack. Meeting Paper AIAA-1998-2879, 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.
Mackall, D. A. and Pickett, M. D. and Schilling, L. J. and Wagner, C. A. (1988) The NASA Integrated Test Facility and Its Impact on Flight Research. Technical Report NASA TM-100418, Research Engineering, NASA Dryden Flight Research Center.
Mackall, D.A. and Pickett, M.D. and Schilling, L.J. and Wagner, C.A. (1988) The NASA Integrated Test Facility and Its Impact on Flight Research. Meeting Paper AIAA-1988-2095, Research Engineering, NASA Dryden Flight Research Center.
Moore, Archie L. (1986) The Role of a Real-Time Flight Support Facility in Flight Research Programs. Technical Report NASA TM-86805, Research Engineering, NASA Dryden Flight Research Center.
Moore, Archie L. (1986) The Role of a Real-Time Flight Support Facility in Flight Research Programs. Meeting Paper AIAA-1986-0166, Research Engineering, NASA Dryden Flight Research Center.
Clarke, Robert and Burken, John J. and Bosworth, John T. and Bauer, Jeffrey E. (1996) X-29 flight control system: lessons learned, in Advances in Aircraft Flight Control, chapter 13, pages 345-367. Taylor & Francis.
Clarke, Robert and Burken, John J. and Bosworth, John T. and Bauer, Jeffrey E. (1994) X-29 Flight Control System: Lessons Learned. Technical Report NASA TM-4598, Research Engineering, NASA Dryden Flight Research Center.
Clarke, Robert and Burken, John J. and Bosworth, John T. and Bauer, Jeffrey E. (1995) X-29 Flight Control System: Lessons Learned. Conference Presentation AGARD-CP-560, Paper No. 12, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. (1984) X-29 Flight-Research Program. Technical Report NASA TM-86025, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. (1983) X-29 Flight-Research Program. Meeting Paper AIAA-1983-2687, Research Engineering, NASA Dryden Flight Research Center.
Ishmael, Stephen D. and Wierzbanowski, LT. Col. Ted (1985) X-29 Initial Flight Test Results.
Sefic, Walter J. and Cutler, William (1986) X-29A Advanced Technology Demonstrator Program Overview. Meeting Paper AIAA-1986-9727, Research Engineering, NASA Dryden Flight Research Center.
Sims, Robert and McCrosson, Paul and Ryan, Robert and Rivera, Joe (1989) X-29A Aircraft Structural Loads Flight Testing. Technical Report NASA TM-101715, Research Engineering, NASA Dryden Flight Research Center.
Chin, J. and Chacon, V. and Gera, J. (1987) X-29A Flight Control System Performance During Flight Test. Meeting Paper AIAA-1987-2878, Research Engineering, NASA Dryden Flight Research Center.
Trippensee, Gary A. and Lux, David P. (1987) X-29A Forward-Swept-Wing Flight Research Program Status. Technical Report NASA TM-100413, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Wang, Kon-Sheng Charles (1996) X-29A Lateral–Directional Stability and Control Derivatives Extracted From High-Angle-of-Attack Flight Data. Technical Report NASA TP-3664, Research Engineering, NASA Dryden Flight Research Center.
Bowers, Albion H. (1984) X-29A Longitudinal and Directional Force and Moment Supplemental Transonic Wind Tunnel Test Results. Technical Report NASA TM-85909, Research Engineering, NASA Dryden Flight Research Center.
Sefic, Walter J. and Maxwell, Cleo M. (1986) X-29A Technology Demonstrator Flight Test Program Overview. Technical Report NASA TM-86809, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sun Nov 22 18:17:15 PST 2009.
