Flight Test Engineering" SYMPOSIUM PROCEEDINGS. 22nd ANNUAL. "Advancement of. August 5-9, 1991

Transcription

1 22nd ANNUAL SYMPOSIUM PROCEEDINGS "Advancement of Flight Test Engineering" Sheraton West Port Inn St. Louis, MO August 59, 1991 Sponsored by the St. Louis Chapter Society of Flight Test Engineers UB/TIB Hannover

2 FLIGHT TABLE OF CONTENTS SESSION I Chairman: TEST METHODS PART 1 Maren Decolator, Long Island Chapter Development and Testing of a Voice Commanded Recovery System Henry F. Geneczko and Frederick W. Schaefer Grumman Aircraft Systems Division, Calverton, NY 1.11 InFlight Detection of Stagnation, Flow Separation, and Transition Characteristics S.M. Mangalam, M.S. Wusk, and S. Kruppa Analytical Services & Materials, Hampton, VA 1.21 An Enhanced Method for Reducing PowerOn Lift Coefficient Data to PowerOff for MultiEngine Propeller Aircraft Stephanous Fajdjis and Ronald N. Segall Grumman Corporation, Bethpage, NY 1.31 Development of a Personal ComputerBased Approach to Aircraft Parameter Identification Captain Mark S. Erickson and Major Daniel Gleason, Air Force Flight Test Center, Edwards AFB, CA 1.41 AHl/MK66 Engineer Investigation Martin A. Ohrenberg U.S. Army AVSCOM, St. Louis, MO 1.51 Flight Test Research for Longitudinal Oscillations of FT7 Aircraft Chen Yang Jian and Kong Ling Qing Xi'an, People's Republic of China 1.61 SESSION II AVIONICS FLIGHT TESTING Chairman: Bob Evans, Antelope Valley Chapter Test Methods and Results From F16/GPS Integration David Henkel Computer Sciences Corporation, Edwards AFB, CA 2.11 Generic Software Tools for Test and Evaluation of Weapon Delivery Systems Lee S. Gardner, Steven J. Martin, and Derrick A. Nguyen Air Force Flight Test Center, Edwards AFB, CA 2.21 TCAS II Testing Conflicts and Resolutions Kevin M. Caldwell Boeing Commercial Airplane Group, Seattle, WA 2.31 F15E Weapons Accuracy Analysis Methodology Charles C. Guthrie Computer Sciences Corporation, Edwards AFB, CA Captain Peter G. Lambert Air Force Flight Test Center, Edwards AFB, CA 2.41 xi

3 DATA Utilization of the Integration Facility for Avionics Systems Testing in F16 Developmental Test and Evaluation Major Glenn Curtiss and Barry Breen Air Force Flight Test Center, Edwards AFB, CA 2.51 Operational Testing of Auto Flight Systems Beyond the North Pole Roger K. Nicholson and Flash Parlini Boeing Company, Seattle, WA 2.61 SESSION III PROCESSING AND DISPLAY Chairman: Doug Stewart, Los Angeles Chapter The VME Based Ground Station & Display System at MCAIR Bruce A. Taylor McDonnell Aircraft Company, St. Louis, MO 3,11 UC880 Telemetry Relay Airborne Command System (TRACS) Jerome C. Gehrig, William D. Anderson and Stephen C. Williams Naval Air Test Center, Patuxent River, MD 3.21 Distributed RealTime Data Processing for the Northrop/McDonnell Douglas YF23 Prototype Flight Test Program D. Kurt Tippey McDonnell Aircraft Company, St. Louis, MO Donald R. Lewallen Northrop Corporation, Hawthorne, CA 3,31 SESSION IV FLIGHT TEST METHODS PART 2 Chairman: Dean Carico, Patuxent River Chapter United States Navy Ski Jump Experience and Future Applications C. Page Senn, T.C. Lea III, and John W Clark Naval Air Tfest Center, Patuxent River, MD 4.11 Development of High AOA Nose Down Control Margin Guidelines for Relaxed Static Stability Tactical Jet Aircraft J. Lackey and W.G. McNamara Naval Air Test Center, Patuxent River, MD 4.21 Single Engine Testing of the F14A(PLUS) Airplane in the Power Approach Configuration R.J. Harney and LCDR B.W. Jett Naval Air lest Center, Patuxent River, MD 4.31 Aerodynamic Loss of Tail Rotor Effectiveness (LTE) Herman Kolway Naval Air Test Center, Patuxent River, MD 4.41 Flight Testing for Agility Captain Alan Lawless Air Force Flight Test Center, Edwards AFB, CA 4.51 xii

4 Yesterday, OFPEmbedded Fly Improved Performance Engine Integration Into the F15E Georges M. Buatois McDonnell Aircraft Company, St. Louis, MO 4.61 Fatigue Load Spectra Analysis of Y7 Aircraft He Ling, Department of Airworthiness Testing Research, Xi'an, Peoples Republic of China 4.71 SESSION V Chairman: AIRBORNE DATA SYSTEMS AND EQUIPMENT Barry Chernick, Seattle Chapter Common Airborne Instrumentation System Raymond J. Faulstich, Naval Air Test Center, Patuxent River, MD 5.11 Hypersonic Vehicle Flight Test Instrumentation James E. Soller, McDonnell Aircraft Company, St. Louis, MO 5.21 Instrumentation for InFIight Acoustic Measurements in an Engine Inlet Duct of a Fokker 100 Aircraft J.M. Klijn and E.R. Rademaker, National Aerospace Laboratory, Amsterdam, Netherlands 5.31 The Future of Flight Test Instrumentation Carl E. Hoefner, Interstate Electronics Corporation, Anaheim, CA 5.41 Dynamic Core Store Data Capture Mordecai Kehat, Israel Air Force, Jerusalem, Israel 5.51 Flight Testing Today, Tomorrow William G. Schweikhard, Kohlman Systems, Research, Lawrence, KS 5.61 SESSION VI FLIGHT TEST PROGRAM REPORTS Chairman: Franz Josef Enzinger, European Chapter YF22A Prototype Advanced Tactical Fighter Demonstration/Validation Flight Test Program Overview Richard Abrams, Lockheed Aeronautical Systems Company, Los Angeles, CA % Leading Edge Root Extension (LERX) Program Flight Test Operations Donald A. Arbuthnot, McDonnell Aircraft Company, St. Louis, MO 6.21 The EJ 200 Engine Design and Development Status Dr. Harmut Gruber and Jon Bjorvik, MTU MororenOnd Turbinen Union MUnchen, Germany 6.31 Flight Test of the YF23A Advanced Tactical Fighter Paul Metz, Northrop Corporation, Hawthorne CA Presented by Bill Lowe, McDonnell Aircraft Company, St. Louis, MO 6.41 Flight Testing the Space Shuttle Orbiter Michael Engle, NASA, Houston, TX 6.51 xiii

5 Research Through Demonstration: X31 Flight Test David Rodrigues, Rockwell International, Lancaster, CA 6.61 F117 Flight Test Program Richard Abrams and Harold C. Farley, Lockheed Advanced Development Company, Los Angeles, CA 6.71 xlv