Subject: X-31
Number of records: 18.
Ryan III, George W. (1995) A Genetic Search Technique for Identification of Aircraft Departures. Technical Report NASA CR-4688, Research Engineering, NASA Dryden Flight Research Center.
Larson, Richard R. and Millard, D. Edward (1992) A Rule-Based System for Real-Time Analysis of Control Systems. Technical Report NASA TM-104258, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Freudinger, Lawrence C. (1994) Aircraft Ground Vibration Testing at the NASA Dryden Research Facility – 1993. Technical Report NASA TM-104275, Research Engineering, NASA Dryden Flight Research Center.
Cobleigh, Brent R. and Croom, Mark A. (2001) Comparison of X-31 Flight and Ground-Based Yawing Moment Asymmetries at High Angles of Attack. Technical Report NASA/TM-2001-210393, Research Engineering, NASA Dryden Flight Research Center.
Cobleigh, Brent R. and Croom, Mark A. (2003) Comparison of X-31 Flight and Ground-Based Yawing Moment Asymmetries at High Angles of Attack. Meeting Paper (SYA) 42-1, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Cobleigh, Brent R. (1994) Controlling Forebody Asymmetries in Flight—Experience With Boundary Layer Transition Strips. Technical Report NASA TM-4595, Research Engineering, NASA Dryden Flight Research Center.
Stoliker, Patrick C. and Bosworth, John T. (1996) Evaluation of High-Angle-of-Attack Handling Qualities for the X-31A Using Standard Evaluation Maneuvers. Technical Report NASA TM-104322, Research Engineering, NASA Dryden Flight Research Center.
Stoliker, Patrick C. and Bosworth, John T. (1997) Evaluation of High-Angle-of-Attack Handling Qualities for the X-31A Using Standard Evaluation Maneuvers. Conference Presentation AGARD-CP-593, Paper No. 29, Research Engineering, NASA Dryden Flight Research Center.
Cobleigh, Brent R. (1994) High-Angle-of-Attack Yawing Moment Asymmetry of the X-31 Aircraft from Flight Test. Technical Report NASA CR-186030, Research Engineering, NASA Dryden Flight Research Center.
Stoliker, Patrick C. and Bosworth, John T. and Georgie, Jennifer (1997) Linearized Poststall Aerodynamic and Control Law Models of the X-31A Aircraft and Comparison with Flight Data. Technical Report NASA/TM-97-206318, Research Engineering, NASA Dryden Flight Research Center.
Mackall, Dale and Norlin, Kenneth and Cohen, Dorothea and Kellogg, Gary and Schilling, Lawrence and Sheen, John (1992) Rapid Development of the X-31 Simulation to Support Flight-Testing. Technical Report NASA TM-104256, Research Engineering, NASA Dryden Flight Research Center.
Mackall, Dale and Norlin, Kenneth and Cohen, Dorothea and Kellogg, Gary and Schilling, Lawrence and Sheen, John (1992) Rapid Development of the X-31 Simulation to Support Flight-Testing. Meeting Paper AIAA-1992-4176, 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.
Bosworth, John T. and Burken, John J. (1997) Tailored Excitation for Multivariable Stability-Margin Measurement Applied to the X-31A Nonlinear Simulation. Technical Report NASA TM-113085, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. and Stoliker, P. C. (1996) The X-31A Quasi-Tailless Flight Test Results. Technical Report NASA TP-3624, Research Engineering, NASA Dryden Flight Research Center.
Cobleigh, Brent R. and Del Frate, John (1994) Water Tunnel Flow Visualization Study of a 4.4% Scale X-31 Forebody. Technical Report NASA TM-104276, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Mon Nov 23 18:17:20 PST 2009.
