Subject: Nonaircraft-specific
Number of records: 55.
Larson, Terry J. and Ehernberger, L.J. (1985) A Constant Altitude Flight Survey Method for Mapping Atmospheric Ambient Pressures and Systematic Radar Errors. Technical Report NASA TM-86733, Research Engineering, NASA Dryden Flight Research Center.
Maine, Richard E. and Iliff, Kenneth W. (1975) A FORTRAN Program for Determining Aircraft Stability and Control Derivatives From Flight Data. Technical Report NASA Technical Note TN D-7831, Research Engineering, NASA Dryden Flight Research Center.
Diebler, Corey and Smith, Mark (2002) A Ground-Based Research Vehicle for Base Drag Studies at Subsonic Speeds. Technical Report NASA/TM-2002-210737, Research Engineering, NASA Dryden Flight Research Center.
Kempel, Robert W. and McNeill, Walter E. and Gilyard, Glenn B. and Maine, Trindel A. (1988) A Piloted Evaluation of an Oblique-Wing Research Aircraft Motion Simulation With Decoupling Control Laws. Technical Report NASA TP-2874, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Kuhl, Albert E. (1977) A Study of the Effect of Radical Load Distributions on Calibrated Strain Gage Load Equations. Technical Report NASA TM-56047, Research Engineering, NASA Dryden Flight Research Center.
Sakamoto, Glenn M. (1976) Aerodynamic Characteristics of a Vane Flow Angularity Sensor System Capable of Measuring Flightpath Accelerations for the Mach Number Range From 0.40 to 2.54. Technical Report NASA Technical Note TN D-8242, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. (1988) Aircraft Flight Flutter Testing at the NASA Ames-Dryden Flight Research Facility. Technical Report NASA TM-100417, Research Engineering, NASA Dryden Flight Research Center.
Weil, Joseph and Day, Richard E. (1956) An Analog Study of the Relative Importance of Various Factors Affecting Roll Coupling. Technical Report NACA RM H56A06, Research Engineering, NASA Dryden Flight Research Center.
Veatch, Donald W. and Bogue, Rodney K. (1986) Analog Signal Conditioning for Flight-Test Instrumentation. Technical Report NASA Reference Publication RP-1159, Research 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.
Sarrafian, Shahan K. and Powers, Bruce G. (1985) Application of Frequency Domain Handling Qualities Criteria to the Longitudinal Landing Task. Technical Report NASA TM-86728, Research Engineering, NASA Dryden Flight Research Center.
Maine, Richard E. and Iliff, Kenneth W. (1986) Application of Parameter Estimation to Aircraft Stability and Control – The Output-Error Approach. Technical Report NASA Reference Publication RP-1168, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. (1986) Bibliography for Aircraft Parameter Estimation. Technical Report NASA TM-86804, Research Engineering, NASA Dryden Flight Research Center.
Fields, Roger A. and Richards, W. Lance and DeAngelis, V. Michael (2004) Combined Loads Test Fixture for Thermal-Structural Testing Aerospace Vehicle Panel Concepts. Technical Report NASA/TM-2004-212039, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Leondes, Cornelius T. (1990) Compensating for Pneumatic Distortion in Pressure Sensing Devices. Technical Report NASA TM-101716, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Jackson, Raymond H. (1993) Compressive and Shear Buckling Analysis of Metal Matrix Composite Sandwich Panels Under Different Thermal Environments. Technical Report NASA TM-4492, Research Engineering, NASA Dryden Flight Research Center.
Weil, Joseph and Day, Richard E. (1956) Correlation of Flight and Analog Investigations of Roll Coupling. Technical Report NACA RM H56F08, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1979) Correlation of Predicted and Measured Thermal Stresses on an Advanced Aircraft Structure with Dissimilar Materials. Technical Report NASA TM-72865, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Antoniewicz, Robert F. and Krambeer, Keith D. (1988) Derivation and Definition of a Linear Aircraft Model. Technical Report NASA Reference Publication RP-1207, Research Engineering, NASA Ames Research Center Dryden Flight Research Facility.
Duke, Eugene L. and Regenie, Victoria A. (1985) Description of an Experimental Expert System Flight Status Monitor. Technical Report NASA TM-86791, Research Engineering, NASA Dryden Flight Research Center.
Regenie, Victoria A. and Duke, Eugene L. (1985) Design of an Expert-System Flight Status Monitor. Technical Report NASA TM-86739, Research Engineering, NASA Dryden Flight Research Center.
Potter, Starr and Lind, Rick (2001) Developing Uncertainty Models for Robust Flutter Analysis Using Ground Vibration Test Data. Technical Report NASA/TM-2001-210392, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Antoniewicz, Robert F. (1985) Development and Validation of a General Purpose Linearization Program for Rigid Aircraft Models. Technical Report NASA TM-86737, Research Engineering, NASA Dryden Flight Research Center.
Peterson, Randall L. (1981) Drag Reduction Obtained by the Addition of a Boattail to a Box Shaped Vehicle. Technical Report NASA CR-163113, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1980) Elastic Constants for Superplastically Formed/Diffusion-Bonded Corrugated Sandwich Core. Technical Report NASA TP-1562, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Lindsey, William T. and Curry, Robert E. and Gilyard, Glenn B. (1990) Experimental Characterization of the Effects of Pneumatic Tubing on Unsteady Pressure Measurements. Technical Report NASA TM-4171, Research Engineering, NASA Dryden Flight Research Center.
Hakkinen, Raimo J. and Neubauer, Jeremy S. and Hamory, Philip J. and Bui, Trong T. and Noffz, Gregory K. (2003) Exploratory Calibration of Adjustable-Protrusion Surface-Obstacle (APSO) Skin Friction Vector Gage. Technical Report NASA/TM-2003-210739, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. (1985) Extraction of Aerodynamic Parameters for Aircraft at Extreme Flight Conditions. Technical Report NASA TM-86730, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. and Gilyard, Glenn B. (1989) Flight Evaluation of a Pneumatic System for Unsteady Pressure Measurements Using Conventional Sensors. Technical Report NASA TM-4131, Research Engineering, NASA Dryden Flight Research Center.
Weil, Joseph and Gates Jr., Ordway B. and Banner, Richard D. and Kuhl, Albert E. (1955) Flight Experience of Inertia Coupling in Rolling Maneuvers. Technical Report NACA RM H55E17b, Research Engineering, NASA Dryden Flight Research Center.
Beeler, De E. and Bellman, Donald R. and Saltzman, Edwin J. (1956) Flight Techniques for Determining Airplane Drag at High Mach Numbers. Technical Report NACA TN 3821, Research Engineering, NASA Dryden Flight Research Center.
Horton, Timothy W. and Kempel, Robert W. (1988) Flight Test Experience and Controlled Impact of a Remotely Piloted Jet Transport Aircraft. Technical Report NASA TM-4084, Research Engineering, NASA Dryden Flight Research Center.
Gupta, Naren K. and Iliff, Kenneth W. (1985) Identification of Unsteady Aerodynamics and Aeroelastic Integro-Differential Systems. Technical Report NASA TM-86749, Research Engineering, NASA Dryden Flight Research Center.
Goecke Powers, Sheryll (1988) Influence of Base Modifications on In-Flight Base Drag in the Presence of Jet Exhaust for Mach Numbers From 0.7 to 1.5. Technical Report NASA TP-2802, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Gilyard, Glenn B. and Gelhausen, Paul A. (1990) Integrated Flight-Propulsion Control Concepts for Supersonic Transport Airplanes. Technical Report NASA TM-101728, Research Engineering, NASA Dryden Flight Research Center.
Nissim, E. and Gilyard, Glenn B. (1989) Method for Experimental Determination of Flutter Speed by Parameter Identification. Technical Report NASA TP-2923, Research Engineering, NASA Dryden Flight Research Center.
Sefic, Walter J. and Anderson, Karl F. (1969) NASA High Temperature Loads Calibration Laboratory. Technical Report NASA TM X-1868, Research Engineering, NASA Dryden Flight Research Center.
Schuster, Lawrence S. (1984) NASTRAN/FLEXSTAB Procedure for Static Aeroelastic Analysis. Technical Report NASA TM-84897, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Bolonkin, Alexander (2000) Optimal Pitch Thrust-Vector Angle and Benefits for all Flight Regimes. Technical Report NASA/TM-2000-209021, Research Engineering, NASA Dryden Flight Research Center.
Pahle, Joseph W. (1990) Output Model-Following Control Synthesis for an Oblique-Wing Aircraft. Technical Report NASA TM-100454, Research Engineering, NASA Dryden Flight Research Center.
Shafer, Mary F. and Steinmetz, Paul (2001) Pilot-Induced Oscillation Research: Status at the End of the Century. Conference Proceedings Report NASA/CP-2001-210389/VOL1, Pilot-Induced Oscillation Research: The Status at the End of the Century, NASA Dryden Flight Research Center.
Shafer, Mary F. and Steinmetz, Paul (2001) Pilot-Induced Oscillation Research: Status at the End of the Century. Conference Proceedings Report NASA/CP-2001-210389/VOL3, Pilot-Induced Oscillation Research: Status at the End of the Century, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. (1976) Practical Aspects of Using a Maximum Likelihood Estimation Method to Extract Stability and Control Derivatives From Flight Data. Technical Report NASA Technical Note TN D-8209, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Lemcoe, M. M. (1977) Problems Associated with Attaching Strain Gages to Titanium Alloy Ti-6Al-4V. Technical Report NASA TM X-56044, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Regenie, Victoria A. and Deets, Dwain A. (1986) Rapid Prototyping Facility for Flight Research in Artificial-Intelligence-Based Flight Systems Concepts. Technical Report NASA TM-88268, 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.
Williams, Walter C. and Phillips, William H. (1956) Some Recent Research on the Handling Qualities of Airplanes. Technical Report NACA RM H55L29a, Research Engineering, NASA Dryden Flight Research Center.
Gupta, K.K. (1984) STARS - A General-Purpose Finite Element Computer Program for Analysis of Engineering Structures. Technical Report NASA RP-1129, Research Engineering, NASA Dryden Flight Research Center.
Abbott, Larry W. (1984) Test Experience on an Ultrareliable Computer Communication Network. Technical Report NASA TM-85915, Research Engineering, NASA Dryden Flight Research Center.
Glover, Richard D. and O'Neill-Rood, Nora (1989) The Aerospace Energy Systems Laboratory: Hardware and Software Implementation. Technical Report NASA TM-101706, Research Engineering, NASA Dryden Flight Research Center.
Chiles, Harry R. (1988) The Design and Use of a Temperature-Compensated Hot-Film Anemometer System for Boundary-Layer Flow Transition Detection on Supersonic Aircraft. Technical Report NASA TM-100421, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1980) The Effect of Thermal Stresses on the Integrity of Three Built-Up Aircraft Structures. Technical Report NASA TM-81352, Research Engineering, NASA Dryden Flight Research Center.
Nissim, E. (1990) The Effectiveness of Vane-Aileron Excitation in the Experimental Determination of Flutter Speed by Parameter Identification. Technical Report NASA TP-2971, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Kuhl, Albert E. and Carter, Alan L. (1977) The Use of a Simplified Structural Model as an Aid in the Strain Gage Calibration of a Complex Wing. Technical Report NASA TM 56046, Research Engineering, NASA Dryden Flight Research Center.
Moore, Archie L. (1985) The Western Aeronautical Test Range of NASA Ames Research Center. Technical Report NASA TM-85924, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sun Nov 22 18:16:50 PST 2009.
