Subject: (07) Aircraft Propulsion And Power
Number of records: 94.
Johnston, Richard P. (1992) A Preliminary Design and Analysis of an Advanced Heat-Rejection System for an Extreme Altitude Advanced Variable Cycle Diesel Engine Installed in a High-Altitude Advanced Research Platform. Technical Report NASA CR-186021, Research Engineering, NASA Dryden Flight Research Center.
Alag, Gurbux S. and Gilyard, Glenn B. (1990) A Proposed Kalman Filter Algorithm for Estimation of Unmeasured Output Variables for an F100 Turbofan Engine. Technical Report NASA TM-4234, Research Engineering, NASA Dryden Flight Research Center.
Lambert, Heather H. (1991) A Simulation Study of Turbofan Engine Deterioration Estimation Using Kalman Filtering Techniques. Technical Report NASA TM-104233, Research Engineering, NASA Dryden Flight Research Center.
Licata, Stephen J. and Burcham Jr., Frank W. (1983) Airstart Performance of a Digital Electronic Engine Control System in an F-15 Airplane. Technical Report NASA TM-84908, Research and Engineering, NASA Dryden Flight Research Center.
Burcham, Frank W. (1984) Airstart Performance of a Digital Electronic Engine Control System on an F100 Engine.
Steenken, William G. and Williams, John G. and Yuhas, Andrew J. and Walsh, Kevin R. (1997) An Inlet Distortion Assessment During Aircraft Departures at High Angle of Attack for an F/A-18A Aircraft. Technical Report NASA TM-104328, 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.
Walton, James T. and Burcham Jr., Frank W. (1986) Augmentor Performance of an F100 Engine Model Derivative Engine in an F-15 Airplane. Technical Report NASA TM-86745, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Pai, G. David (1984) Augmentor Transient Capability of an F100 Engine Equipped With a Digital Electronic Engine Control .
Johnson, J. Blair (1984) Backup Control Airstart Performance on a Digital Electronic Engine Control-Equipped F100 Engine.
Kurtenbach, Frank J. (1978) Comparison of Calculated and Altitude-Facility-Measured Thrust and Airflow of Two Prototype F100 Turbofan Engines. Technical Report NASA Technical Paper TP-1373, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. and Burcham Jr., Frank W. (1983) Comparison of Flight Results With Digital Simulation for a Digital Electronic Engine Control in an F-15 Airplane. Technical Report NASA TM-84903, Research and Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Vachon, Michael Jacob (2006) Design and Flight Evaluation of a New Force-Based Flow Angle Probe. Technical Report NASA/TM-2006-213673, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and DeLaat, John C. and Southwick, Robert D. and Gallops, George W. and Doane, Paul M. (1998) Development and Testing of a High Stability Engine Control (HISTEC) System. Technical Report NASA/TM-1998-206562, Research Engineering, NASA Dryden Flight Research Center.
Authors, Various (1984) Digital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane. Technical Report NASA Conference Publication CP-2298, Research Engineering, NASA Dryden Flight Research Center.
Kock, Berwin (1984) Digital Electronic Engine Control F-15 Overview.
Baer-Riedhart, Jennifer L. (1984) Digital Electronic Engine Control Fault Detection and Accommodation Flight Evaluation.
Putnam, Terrill W. (1984) Digital Electronic Engine Control History.
Martin, Richard A. (1970) Dynamic Analysis of XB-70-1 Inlet Pressure Fluctuations During Takeoff and Prior to a Compressor Stall at Mach 2.5. Technical Report NASA Technical Note TN D-5826, Research Engineering, NASA Dryden Flight Research Center.
Norby, W. P. and Ladd, J. A. and Yuhas, A. J. (1996) Dynamic Inlet Distortion Prediction with a Combined Computational Fluid Dynamics and Distortion Synthesis Approach. Technical Report NASA CR-198053, Research Engineering, NASA Dryden Flight Research Center.
Crawford, David B. and Burcham Jr., Frank W. (1984) Effect of Control Logic Modifications on Airstart Performance of F100 Engine Model Derivative Engines in an F-15 Airplane. Technical Report NASA TM-85900, Research Engineering, NASA Dryden Flight Research Center.
Stoll, Frederick and Tremback, Jeffrey W. and Arnaiz, Henry H. (1979) Effect of Number of Probes and Their Orientation on the Calculation of Several Compressor Face Distortion Descriptors. Technical Report NASA TM-72859, Research Engineering, NASA Dryden Flight Research Center.
Yuhas, Andrew J. and Ray, Ronald J. (1992) Effects of Bleed Air Extraction on Thrust Levels of the F404-GE-400 Turbofan Engine. Technical Report NASA TM-104247, Research Engineering, NASA Dryden Flight Research Center.
Hughes, Donald L. and Mackall, Karen G. (1984) Effects of Inlet Distortion on a Static Pressure Probe Mounted on the Engine Hub in an F-15 Airplane.
Hughes, Donald L. and Myers, Lawrence P. and Mackall, Karen G. (1985) Effects of Inlet Distortion on a Static Pressure Probe Mounted on the Engine Hub in an F-15 Airplane. Technical Report NASA TP-2411, Research Engineering, NASA Dryden Flight Research Center.
Ennix, Kimberly A. (1993) Engine Exhaust Characteristics Evaluation in Support of Acoustic Testing. Technical Report NASA TM-104263, Research Engineering, NASA Dryden Flight Research Center.
Williams, J. G. and Steenken, W. G. and Yuhas, A. J. (1996) Estimating Engine Airflow in Gas-Turbine Powered Aircraft With Clean and Distorted Inlet Flows. Technical Report NASA CR-198052, 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.
Kurtenbach, Frank J. (1979) Evaluation of a Simplified Gross Thrust Calculation Technique Using Two Prototype F100 Turbofan Engines in an Altitude Facility. Technical Report NASA Technical Paper TP-1482, Research Engineering, NASA Dryden Flight Research Center.
Jones, Thomas P. and Baumann, Ethan (2003) Evaluation of the X-43A Scramjet Engine Controller Performance by Monte Carlo Technique. Technical Report NASA/TM-2003-212036, Research Engineering, NASA Dryden Flight Research Center.
Walton, James T. and Burcham Jr., Frank W. (1986) Exhaust-Gas Pressure and Temperature Survey of F404-GE-400 Turbofan Engine. Technical Report NASA TM-88273, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. (1984) F-15 Digital Electronic Engine Control System Description.
Yuhas, Andrew J. and Steenken, William G. and Williams, John G. and Walsh, Kevin R. (1997) F/A-18A Inlet Flow Characteristics During Maneuvers with Rapidly Changing Angle of Attack. Technical Report NASA TM-104327, Research Engineering, NASA Dryden Flight Research Center.
Steenken, W. G. and Williams, J. G. and Yuhas, A. J. and Walsh, K. R. (1999) Factors Affecting Inlet-Engine Compatibility During Aircraft Departures at High Angle of Attack for an F/A-18A Aircraft. Technical Report NASA/TM-1999-206572, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. and Baer-Riedhart, Jennifer L. and Maxwell, Michael D. (1985) Fault Detection and Accommodation Testing on an F100 Engine in an F-15 Airplane. Technical Report NASA TM-86735, Research Engineering, NASA Dryden Flight Research Center.
Holzman, Jon K. and Webb, Lannie D. and Burcham Jr., Frank W. (1996) Flight and Static Exhaust Flow Properties of an F110-GE-129 Engine in an F-16XL Airplane During Acoustic Tests. Technical Report NASA TM-104326, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and Schkolnik, Gerard S. (1995) Flight Assessment of the Onboard Propulsion System Model for the Performance Seeking Control Algorithm on an F-15 Aircraft. Technical Report NASA TM-4705, Research Engineering, NASA Dryden Flight Research Center.
Walsh, Kevin R. and Burcham, Frank W. (1984) Flight Evaluation of a Hydromechanical Backup Control for the Digital electronic Engine Control System in an F100 Engine.
Kurtenbach, Frank J. and Burcham Jr., Frank W. (1981) Flight Evaluation of a Simplified Gross Thrust Calculation Technique Using an F100 Turbofan Engine in an F-15 Airplane. Technical Report NASA TP-1782, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. and Conners, Timothy R. (1992) Flight Evaluation of an Extended Engine Life Mode on an F-15 Airplane. Technical Report NASA TM-104240, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Myers, Lawrence P. (1983) Flight Evaluation of Modifications to a Digital Electronic Engine Control System in an F-15 Airplane. Technical Report NASA TM-83088, Research and Engineering, NASA Dryden Flight Research Center.
Johnson, J. Blair and Nelson, Jeff (1983) Flight Evaluation of the DEEC Secondary Engine Control Airstart Capability. Technical Report NASA TM-84910, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Myers, Lawrence P. and Walsh, Kevin R. (1983) Flight Evaluation Results for a Digital Electronic Engine Control in an F-15 Airplane . Technical Report NASA TM-84918, Research and Engineering, NASA Dryden Flight Research Center.
Hernandez, Francisco J. and Burcham Jr., Frank W. (1988) Flight Measured and Calculated Exhaust Jet Conditions for an F100 Engine in an F-15 Airplane. Technical Report NASA TM-100419, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. (1984) Flight Testing the Digital Electronic Engine Control in the F-15 Airplane.
Corda, Stephen and Neal, Bradford A. and Moes, Timothy R. and Cox, Timothy H. and Monaghan, Richard C. and Voelker, Leonard S. and Corpening, Griffin P. and Larson, Richard R. and Powers, Bruce G. (1998) Flight Testing the Linear Aerospike SR-71 Experiment (LASRE). Technical Report NASA/TM-1998-206567, 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.
Ennix, Kimberly A. and Burcham Jr., Frank W. and Webb, Lannie D. (1993) Flight-Determined Engine Exhaust Characteristics of an F404 Engine in an F-18 Airplane. Technical Report NASA TM-4538, Research Engineering, NASA Dryden Flight Research Center.
Ray, J.K. and Carlin, C.M. and Lambregts, A.A. (1992) High-Speed Civil Transport Flight- and Propulsion-Control Technological Issues. Technical Report NASA CR-186015, Research Engineering, NASA Dryden Flight Research Center.
Baer-Riedhart, Jennifer L. and Landy, Robert J. (1987) Highly Integrated Digital Electronic Control - Digital Flight Control, Aircraft Model Identification, and Adaptive Engine Control. Technical Report NASA TM-86793, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Haering Jr., Edward A. (1984) Highly Integrated Digital Engine Control System in an F-15 Airplane. Technical Report NASA TM-86040, Research Engineering, NASA Dryden Flight Research Center.
Schkolnik, Gerard S. (1993) Identification of Integrated Airframe–Propulsion Effects on an F-15 Aircraft for Application to Drag Minimization. Technical Report NASA TM-4532, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and Hathaway, Ross and Ferguson, Michael D. (1998) Initial Flight Test Evaluation of the F-15 ACTIVE Axisymmetric Vectoring Nozzle Performance. Technical Report NASA/TM-1998-206558, Research Engineering, NASA Dryden Flight Research Center.
Palumbo, Nathan and Moes, Timothy R. and Vachon, M. Jake (2002) Initial Flight Tests of the NASA F-15B Propulsion Flight Test Fixture. Technical Report NASA/TM-2002-210736, Research Engineering, NASA Dryden Flight Research Center.
Walsh, Kevin R. and Yuhas, Andrew J. and Williams, John G. and Steenken, William G. (1997) Inlet Distortion for an F/A-18A Aircraft During Steady Aerodynamic Conditions up to 60° Angle of Attack. Technical Report NASA TM-104329, Research Engineering, NASA Dryden Flight Research Center.
Walsh, Kevin R. and Yuhas, Andrew J. and Williams, John G. and Steenken, William G. (1996) Inlet Distortion for an F/A-18A Aircraft During Steady Aerodynamic Conditions up to 60º Angle of Attack. In Proceedings High-Angle-of-Attack Technology Conference, pages 1083-1126, NASA Langley Research Center, Hampton, Virginia.
Steenken, William G. and Williams, John G. and Walsh, Kevin R. (1999) Inlet Flow Characteristics During Rapid Maneuvers for an F/A-18A Aircraft. Technical Report NASA/TM-1999-206587, Research Engineering, NASA Dryden Flight Research Center.
Stewart, James F. (1992) Integrated Flight Propulsion Control Research Results Using the NASA F-15 HIDEC Flight Research Facility. Technical Report NASA TM-4394, Research Engineering, NASA Dryden Flight Research Center.
Gallagher, Robert J. (1970) Investigation of a Digital Simulation of the XB-70 Inlet and its Application to Flight-Experienced Free-Stream Disturbances at Mach Numbers of 2.4 to 2.6. Technical Report NASA Technical Note TN D-5827, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Zeller, John R. (1984) Investigation of a Nozzle Instability on an F100 Engine Equipped With a Digital Electronic Engine Control.
Vachon, Michael Jacob and Moes, Timothy R. and Corda, Stephen (2005) Local Flow Conditions for Propulsion Experiments on the NASA F-15B Propulsion Flight Test Fixture. Technical Report NASA/TM-2005-213670, 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.
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.
Bui, Trong T. and Lux, David P. and Stenger, Michael T. and Munson, Michael J. and Teate, George F. (2007) New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic Systems. Technical Report NASA/TM-2007-214624, Research and Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. and Lux, David P. and Stenger, Michael T. and Munson, Michael J. and Teate, George F. (2006) New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic Systems. Meeting Paper AIAA-2006-221, Research Engineering, NASA Dryden Flight Research Center.
España, Martin D. and Gilyard, Glenn B. (1993) On the Estimation Algorithm Used in Adaptive Performance Optimization of Turbofan Engines. Technical Report NASA TM-4551, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. and Burcham Jr., Frank W. and Andries, Mary G. and Kelly, James B. (1985) Performance Improvements of a Highly Integrated Digital Electronic Control System for an F-15 Airplane. Technical Report NASA TM-86748, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. and Walsh, Kevin R. (1988) Performance Improvements of an F-15 Airplane with an Integrated Engine-Flight Control System. Technical Report NASA TM-100431, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Orme, John S. (1993) Performance Seeking Control: Program Overview and Future Directions. Technical Report NASA TM-4531, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Myers, Lawrence P. and Ray, Ronald J. (1985) Predicted Performance Benefits of an Adaptive Digital Engine Control System on an F-15 Airplane. Technical Report NASA TM-85916, Research Engineering, NASA Dryden Flight Research Center.
Lambert, H.H. and Gilyard, G.B. and Chisholm, J.D. and Kerr, L.J. (1991) Preliminary Flight Evaluation of an Engine Performance Optimization Algorithm. Technical Report NASA TM-4328, Research Engineering, NASA Dryden Flight Research Center.
Cho, Tony K. and Burcham Jr., Frank W. (1984) Preliminary Flight Evaluation of F100 Engine Model Derivative Airstart Capability in an F-15 Airplane. Technical Report NASA TM-86031, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. and Burcham Jr., Frank W. (1984) Preliminary Flight Test Results of the F100 EMD Engine in an F-15 Airplane. Technical Report NASA-TM-85902, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and Gilyard, Glenn B. (1993) Preliminary Supersonic Flight Test Evaluation of Performance Seeking Control. Technical Report NASA TM-4494, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. and Burcham Jr., Frank W. (1984) Propulsion Control Experience Used in the Highly Integrated Digital Electronic Control (HIDEC) Program. Technical Report NASA TM-85914, 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 Gilyard, Glenn B. and Myers, Lawrence P. (1990) Propulsion System/Flight Control Integration and Optimization—Flight Evaluation and Technology Transition. Technical Report NASA TM-4207, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and Sims, Robert L. (1999) Selected Performance Measurements of the F-15 ACTIVE Axisymmetric Thrust-Vectoring Nozzle. Meeting Paper ISABE Paper IS-166, 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.
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.
Gilyard, Glenn B. and Orme, John S. (1992) Subsonic Flight Test Evaluation of a Performance Seeking Control Algorithm on an F-15 Airplane. Technical Report NASA TM-4400, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and Gilyard, Glenn B. (1992) Subsonic Flight Test Evaluation of a Propulsion System Parameter Estimation Process for the F100 Engine. Technical Report NASA TM-4426, Research Engineering, NASA Dryden Flight Research Center.
Walsh, Kevin R. (1993) Summary of the Effects of Engine Throttle Response on Airplane Formation-Flying Qualities. Technical Report NASA TM-4465, Research Engineering, NASA Dryden Flight Research Center.
Ray, Ronald J. and Myers, Lawrence P. (1986) Test and Evaluation of the HIDEC Engine Uptrim Algorithm. Technical Report NASA TM-88262, Research Engineering, NASA Dryden Flight Research Center.
Schweikhard, W. G. (1974) Test Techniques, Instrumentation, and Data Processing. AGARD Lecture Series No. 72, Research Engineering, NASA Dryden Flight Research Center.
Evans, Alison B. (1991) The Effects of Compressor Seventh-Stage Bleed Air Extraction on Performance of the F100-PW-220 Afterburning Turbofan Engine. Technical Report NASA CR-179447, Research Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Vachon, M. Jake and Palumbo, Nathan and Diebler, Corey and Tseng, Ting and Ginn, Anthony and Richwine, David (2001) The F-15B Propulsion Flight Test Fixture: A New Flight Facility For Propulsion Research. Technical Report NASA/TM-2001-210395, Research Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Vachon, M. Jake and Palumbo, Nathan and Diebler, Corey and Tseng, Ting and Ginn, Anthony and Richwine, David (2001) The F-15B Propulsion Flight Test Fixture: A New Flight Facility for Propulsion Research. Meeting Paper AIAA-2001-3303, Research Engineering, NASA Dryden Flight Research Center.
Neal, Bradford and Sengupta, Upal (1989) The Implementation and Operation of a Variable-Response Electronic Throttle Control System for a TF-104G Aircraft. Technical Report NASA TM-101696, Research Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Moes, Timothy R. and Mizukami, Masashi and Hass, Neal E. and Jones, Daniel and Monaghan, Richard C. and Ray, Ronald J. and Jarvis, Michele L. and Palumbo, Nathan (2000) The SR-71 Test Bed Aircraft: A Facility for High-Speed Flight Research. Technical Report NASA/TP-2000-209023, Research Engineering, NASA Dryden Flight Research Center.
Soreide, David and Bogue, Rodney K. and Seidel, Jonathan and Ehernberger, L.J. (1997) The Use of a Lidar Forward-Looking Turbulence Sensor for Mixed Compression Inlet Unstart Avoidance and Gross Weight Reduction on a High Speed Civil Transport. Technical Report NASA TM-104332, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Ray, Ronald J. (1987) The Value of Early Flight Evaluation of Propulsion Concepts Using the NASA F-15 Research Airplane. Technical Report NASA TM-100408, Research Engineering, NASA Dryden Flight Research Center.
Conners, Timothy R. (1992) Thrust Stand Evaluation of Engine Performance Improvement Algorithms in an F-15 Airplane. Technical Report NASA TM-104252, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. and Smith, Ronald H. (1970) XB-70 Compressor-Noise Reduction and Propulsion-System Performance For Choked Inlet Flow. Technical Report NASA Technical Note TN D-5692, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sat Nov 21 18:15:26 PST 2009.
