Document waKK7XM9d1bmroYZoDqeKLv3

AIRCRAFT PROPULSION 670,064 Shaft, Bearing, and Seal Systems for a Small Engine - R. P. Shevchenko, United Aircraft 67013B An Approach to Simpler Control Requirements - D. E. Uehllng, GE 670139 Some Aspects of the Control of Multi-Shaft Jet Engines - W. G. Cross and W. B. Edwards, RollsRoyce 670140 Some Aircraft Gas Turbine Environ mental Challenges for the Fuel Control Designer - L. J. Moulton, GE 670141 PresentNeeds of Gas Turbine Control Systems and Predictions for the Future - P. M. Slade and J. B. Eastman, Boeing 670142 Controls for Gas Turbines Used as Centrifugal Compressor Drivers H. 0. Lena, Cooper Bessemer 670194 The Rotating Combustion Engine Compact, Lightweight Power for Air craft - Charles Jones, CurtissWright 670198 The Performance of Vehicle Gas Turbines - D. E. Barbeau, Contin ental Avia, and Enffg. 670234 Designing Business Jet Aircraft Engines for Increased Service Life - F. W. Garry, General Electric 670235 Thrust Reversers for Business Jet Aircraft-J. C. PickerdandC. M. Hinds, Rohr 670236 Growth and Operational Capabili ties of the Turboprop Engine - H. A. Buckner, R. R. VanNimwegen, AiResearch Mfg. 670237 The General Problems in Vibra tion of Aircraft Powerplant Compo nents - E. F. Critchlow, Consul tant (Formerly with Federal Avia tion Agenctf 670238 Two-Stroke Light-Aircraft Engine Potential - J. L. Dooley, McCul loch 670267 Powerplant Pressurization for Altitude - Don Trompler and J. B. O'Reilly, Mooney Aircraft 670325 Operating Techniques and Main tenance Considerations for Air Inlet Controls in Airline Service R. D. Porter, United Aircraft 670326 Fuel Control System of the GE4 Engine for the Supersonic Trans port - J. T. Moehring, GE 670330 Maintainability Design Require ments for Future Jet Engines J. J. Morel I i, TWA 670331 Designing the JT9D to Meet Commercial Transport Require ments - J. D. Kester and T. G. Slaiby, United Aircraft 670332 AELCEF--A Tool to make Rotor Burst Containment a Reality A. A. Martino and G. J. Mangano, Naval Air Engrg. Cen. 670334 T63 Engine Sand and Dust Tol erance, Development and Field Experience - G. V. Bianchini, All|son Div., GMC 670344 Design Criteria and Configuration for Long-Life Aircraft Gas Tur bines - J. S. Alford, GE 670345 Development of a High Temperature, Long-Life Turbine - W. W. Jones, Allison Div., GMC 670347 A New Concept for Critical Speed Control - M. R. Kulina, J. F. Mullen, M. Natesh, and H. W. Saltzman, Curtiss-Wright 670353 Adam II Propulsion System and Internal Aerodynamics - C. T. Havey, LTV Aerospace 670354 Mixed Missions--Potential Improvements in Thermal Manage ment of Hypersonic Designs - C. J. MacMiller, North Amer. Avia., Inc. 670358 One Airline's Hits and Misses in Propulsion Systems Diagnostics - J. N. Smith, Air Canada 670359 U.S.A.F. Application of Air borne Recorders for Propulsion Diagnostics -R. J. Carlson, Air Force Systems Command 670363 Designing Diagnostics Into Propul sion Systems - J. C. Pirtle, GE 670838 Design and Transient Performance of a Liquid Coolant System - R. S. Barker, H. M. Stephens, and B. N. Taylor, Douglas Aircraft 670865 An Airline View of the SST Powerplants - F. Searls, United Air Lines 670871 A Jet Engine Malfunction Diagnostic System Using Sonic/Vibration Analysis - A. J. Kasak and L. R. Last, GE 670872 Engine Vibration Signals as an Aid to Fault Diagnosis - L. R. Hulls and J. R. Welch, Philco-Ford 670873 Mechanical Impedance Approach to Engine Vibration Transmission Into an Aircraft Fuselage - S. Rubin, Aerospace Corn.,- and F. A. Biehl, McDonnell Douglas 670874 Applications of Fast Fourier Trans form Procedures to Shock and Vibra tion Data Analysis - L. D. Enochson and A. G. Piersol. Measurement Analysis 680224 The Allison 250 Turboprop, Development and Application J. M. Wetzler and R. L. Chaney, Allison Div., GMC 4 680226 Performance Characteristics of Air craft with Turbosupercharged Engine & Cabin--1968 - D. L. Satchwell, Garrett * 680227 Propeller Design Considerations for Turbine Powered Aircraft - D. P. Currie, United Aircraft 680229 Applications of Automotive Elec trical Equipment in Light Aircraft Engines-D. P. Hansen and C. R. Goulet, Continental Motors *680230 The Beechcraft 99 - C. A. Rembleske, Chief Tech. Engr., Beech Aircraft Corp. 680276 The Commercial Transport Manu facturer's Position -W. A. Rein hart and G. J. Schott, Boeing 680277 The Military Outlook for Adaptive Propulsion Systems -H. I. Bush, USAF Aero Propulsion Lab. 680278 The Engine Manufacturer's Outlook W. H. Sens and R. M. Meyer, United Aircraft 680279 Research Problems and Outlook N. F. Rekos, Aeronautical Ve hicles Div., NASA 680286 An Engine Man's Point of View on Integration of Inlet and Engine H. N. Cotter, United Aircraft *680287 An Airplane Man's Point of View on Integration of Inlet and Engine L. M. Randall, Supv. andW. H. Hand, N. Amer. Rockwell * 680288 Airframe-Propulsion Integration for Future Aircraft Systems - G. K. Richey, D. J. Stava, B. Brimelow and H. I. Bush, U. S. Air Force Systems Command 680294 Optimizing Exhaust Nozzle/Airframe Thrust Minus Dray - D. Migdal and W. K. Greathouse, Grumman *680295 Variable-Geometry Exhaust Nozzles and Their Effects on Airplane Per formance -W. F. Punch and R. C. Ammer, General Electric *680296 Performance Installation Effects for Nozzles Installed on a Twin Jet Fighter Airplane Model - D. L. Motycka and P. J. Skowronek, United Aircraft *680309 A Variable Speed Constant Fre quency Power Source - William Finn, Lear Jet *680310 Modular Aircraft-Engine Logistics System - R. E. Williams and D. W. Sommer, Vickers 680311 Auxiliary Power Systems for 1975 Fighter Aircraft -B. H. Nicholls, Garrett VPD-81-0001643