Subject: Not Categorized
Number of records: 44.
Deets, Dwain A. and Edwards, John W. (1974) A Remotely Augmented Vehicle Approach to Flight Testing RPV Control Systems. Technical Report NASA TM X-56029, Reseach Engineering, NASA Dryden Flight Research Center.
Edwards, John W. (1972) Analysis of an Electrohydraulic Aircraft Control-Surface Servo and Comparison With Test Results. Technical Report NASA Technical Note TN D-6928, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. (1988) Application of Flight Systems Methodologies to the Validation of Knowledge-Based Systems. Technical Report NASA TM-100442, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. (1982) Automated Flight Test Maneuvers: The Development of a New Technique.
Wolowicz, Chester H. and Yancey, Roxanah B. (1973) Comparison of Predictions of the XB-70-1 Longitudinal Stability and Control Derivatives With Flight Results For Six Flight Conditions. Technical Report NASA TM X-2881, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1979) Criteria for Representing Circular Arc and Sine Wave Spar Webs by Non-Curved Elements. Technical Report NASA TM-72869, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. (1957) Dynamic Longitudinal Stability Characteristics of a Swept-Wing Fighter-Type Airplane at Mach Numbers Between 0.36 and 1.45. Technical Report NACA RM H56H03, Research Engineering, NASA Dryden Flight Research Center.
Monaghan, Richard C. and Fields, Roger A. (1973) Experiments to Study Strain-Gage Load Calibrations on a Wing Structure at Elevated Temperatures. Technical Report NASA Technical Note TN D-7390, Research Engineering, NASA Dryden Flight Research Center.
Andrews, William H. and Robinson, Glenn H. and Larson, Richard R. (1972) Exploratory Flight Investigation of Aircraft Response to The Wing Vortex Wake Generated by Jet Transport Aircraft. Technical Report NASA Technical Note TN D-6655, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. (1999) Fifty Years of Flight Research: An Annotated Bibliography of Technical Publications of NASA Dryden Flight Research Center, 1946–1996. Technical Report NASA/TP-1999-206568, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Dougherty Jr., N. Sam (1983) Flight and Wind-Tunnel Correlation of Boundary-Layer Transition on the ADEC Transition Cone.
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.
Love, James E. and Fox, William J. and Wicklund, Edward J. (1974) Flight Study of a Vehicle Operational Status and Monitoring System. Technical Report NASA Technical Note TN D-7546, Research Engineering, NASA Dryden Flight Research Center.
Painter, Weneth D. (1983) Flight Testing of Unique Aircraft Configurations. AIAA Student Journal 21:2-7, 23.
Smith, Harriet J. (1975) Flight-Determined Stability and Control Derivatives for an Executive Jet Transport. Technical Report NASA TM X-56034, Research Engineering, NASA Dryden Flight Research Center.
Berry, Donald T. (1982) Flying Qualities: A Costly Lapse in Flight-Control Design. Astronautics and Aeronautics 20:54-57.
Maine, Richard E. and Iliff, Kenneth W. (1983) Formulation of a Practical Algorithm For Parameter Estimation With Process and Measurement Noise.
Maine, Richard E. and Iliff, Kenneth W. (1982) Formulation of a Practical Algorithm for Parameter Estimation With Process and Measurement Noise.
Wagner, Charles A. (1970) Frequency Responses and Other Characteristics of Six Fast-Decay Phosphors Applicable to Flying-Spot Scanners. Technical Report NASA Technical Note TN D-6036, 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.
Berry, Donald T. and Powers, Bruce G. and Szalai, Kenneth J. and Wilson, R. J. (1982) In-Flight Evaluation of Control System Pure Time Delays. Journal of Aircraft 19(4):318-323.
Larson, Terry J. and Thomas, George M. and Bellman, Donald R. (1958) Induction System Characteristics and Engine Surge Occurrence for Two Fighter-Type Airplanes. Technical Report NACA RM H58C14, 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.
Curry, Robert E. (1983) Limited Flight Test Experience With a Laser Transit Velocimeter. Technical Report NASA TM-84896, Research and Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Putnam, Terrill W. and Lasagna, Paul L. and Parish, O. Owen (1975) Measured Noise Reductions Resulting from Modified Approach Procedures for Business Jet Aircraft. Technical Report NASA TM X-56037, Research Engineering, NASA Dryden Flight Research Center.
Schneider, Edward T. and Enevoldson, Einar K. (1984) Modernizing Engine Displays.
Szalai, Kenneth J. (1971) Motion Cue and Simulation Fidelity Aspects of the Validation of a General Purpose Airborne Simulator. Technical Report NASA Technical Note TN D-6432, Research Engineering, NASA Dryden Flight Research Center.
Abbott, Larry W. (1983) Operational Characteristics of the Dispersed Sensor Processor Mesh.
Authors, Various (1974) Parameter Estimation Techniques and Applications in Aircraft Flight Testing- A Symposium at The NASA Flight Research Center, April 24-25, 1973. Technical Report NASA Technical Note TN D-7647, Research Engineering, NASA Dryden Flight Research Center .
Strovers, Brian K. and Lee, James A. (2009) Platform Precision Autopilot Overview and Mission Performance.
Putnam, Terrill W. (1975) Review of Aircraft Noise Propagation. Technical Report NASA TM X-56033, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. and Kier, David A. (1973) Simulator Evaluation of the Low-Speed Flying Qualities of an Experimental STOL Configuration With an Externally Blown Flap Wing or an Augmentor Wing. Technical Report NASA Technical Note TN D-7454, Research Engineering, NASA Dryden Flight Research Center.
Holleman, Euclid C. and Stillwell, Wendell H. (1958) Simulator Investigation of Command Reaction Controls. Technical Report NACA RM H58D22, Research Engineering, NASA Dryden Flight Research Center.
Petersen, Kevin L. and Flores Jr., Christobal (1983) Software Control and System Configuration Management: A Process That Works.
Shafer, Mary F. (1975) Stability and Control Derivatives of the T-37B Airplane. Technical Report NASA TM X-56036, Research Engineering, NASA Dryden Flight Research Center.
Albers, James A. (1976) Status of the NASA YF-12 Propulsion Research Program. Technical Report NASA TM X-56039, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1982) Structural Properties of Superplastically Formed, Diffusion-Bonded Orthogonally Corrugated Core Sandwich. AIAA 20(4):536-543.
Maine, Richard E. and Iliff, Kenneth W. (1981) The Theory and Practice of Estimating the Accuracy of Dynamic Flight-Determined Coefficients. Technical Report NASA Research Publication RP-1077, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. (1956) Time-Vector Determined Lateral Derivatives of a Swept-Wing Fighter-Type Airplane with Three Different Vertical Tails at Mach Numbers Between 0.70 and 1.48. Technical Report NACA RM H56C20, Research Engineering, NASA Dryden Flight Research Center.
Lung, Shun-fat and Pak, Chan-gi (2009) Updating the Finite Element Model of the Aerostructures Test Wing Using Ground Vibration Test Data. Meeting Paper, AIAA-2009-2528, Research and Engineering, NASA Dryden Flight Research Center.
Montoya, Lawrence C. and Economu, Merle A. and Cissell, Ralph E. (1974) Use of a Pitot-Static Probe for Determining Wing Section Drag in Flight at Mach Numbers from 0.5 to Approximately 1.0. Technical Report NASA TM X-56025, Research Engineering, NASA Dryden Flight Research Center.
Murray, James E. (1982) User's Manual for THPLOT, A FORTRAN 77 Computer Program for Time History Plotting. Technical Report NASA TM-81374, Research and Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. (1983) Uses of Parameter Estimation in Flight Test. Journal of Aircraft 20(12):1043-1049.
Lewis, Thomas L. and Dods Jr., Jules B. (1972) Wind-Tunnel Measurements of Surface-Pressure Fluctuations at Mach Numbers of 1.6, 2.0, and 2.5 Using 12 Different Transducers. Technical Report NASA Technical Note TN D-7087, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Mon Nov 23 18:16:55 PST 2009.
