1–20 of 226 hits
|

    AIAA-2007-1372 PROPULSION SYSTEM CONCEPTS FOR THE PLANETARY SURVEY MISSIONS

    Futamura, H. / Okai, K. / Yanagi, R. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1341 DESIGN OF A COUNTER-ROTATING TURBINE FOR A HYPERSONIC AIRCRAFT

    Paniagua, G. / Szokol, S. / Kato, H. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1336 MORE INTELLIGENT GAS TURBINE ENGINES

    Stiharu, I. / Horn, W. / Fpoertner, H. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1335 MICRO PRESSURE SENSOR FOR HIGH TEMPERATURE APPLICATIONS

    Leo, A. / Stiharu, I. / Bhat, R.B. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1302 AERODYNAMIC IMPROVEMENT OF LOW PRESSURE TURBINE USING 3D VISCOUS FLOW COMPUTATIONS

    Murthy, S.V.R. / Ganesh, R. / Krishnaiah, T.V. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1299 AERO-THERMAL ANALYSIS OF A PARTIALLY SHROUDED AXIAL TURBINE

    Kalfas, A.I. / Porreca, L. / Abhari, R.S. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1290 ON-WING DECISION SUPPORT FOR AERO-ENGINE LINE REPLACEABLE UNIT FAULT ISOLATION

    Mills, A.R. / Tanner, G. / Thompson, H. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1263 EXPERIMENTAL INVESTIGATION OF ROTATING STALL IN A RESEARCH MULTISTAGE AXIAL COMPRESSOR

    Lepicovsky, J. / Braunscheidel, E.P. / Welch, G.E. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1240 ADVANCED HEAT EXCHANGERS FOR USE WITH AIRCRAFT ENGINES

    Strumpf, H.J. / Muley, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    AIAA-2007-1230 NUMERICAL SIMULATIONS OF FLUID-STRUCTURE INTERACTIONS USING IMMERSED BOUNDARY METHOD

    Zhong, G. / Sun, X. / Liang, A. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1215 A QUASI-ONE-DIMENSIONAL MODEL FOR AXIAL TURBINES

    Adam, O. / Leonard, O. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    AIAA-2007-1164 3D FLOW STRUCTURES ADJACENT RECTANGULAR COOLING HOLES

    Kang, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    AIAA-2007-1125 DESIGN AND VALIDATION OF A REAL-TIME MODEL FOR STEADY-STATE AND TRANSIENT PERFORMANCE SIMULATION OF A HELICOPTER ENGINE

    Frowein, J. / Abdullahi, H. / Erhard, W. et al. | British Library Conference Proceedings | 2007

    AIAA-2007-1110 EFFECT OF T56 PRESWIRL COOLING MODELLING ON DISC ASSEMBLY TEMPERATURE PREDICTION

    Roos, T. / Kruger, E. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    AIAA-2007-1109 NONCONTACT BLADE VIBRATION AND TIP CLEARANCE MEASUREMENT SYSTEM FOR AERO ENGINE APPLICATION

    Zielinski, M. / Ziller, G. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    AIAA-2007-1370 IMPROVING OF A VANED DIFFUSER FOR A GIVEN CENTRIFUGAL IMPELLER BASED ON CFD AND OPTIMIZATION METHOD

    Xi, G. / Wang, Z. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    AIAA-2007-1359 SIMULATION-BASED PERFORMANCE ANALYSIS OF AXISYMMETRIC CASING TREATMENTS IN AXIAL COMPRESORS

    Lepot, I. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    AIAA-2007-1338 A RETRO-FIT CONTROL ARCHITECTURE TO MAINTAIN ENGINE PERFORMANCE WITH USAGE

    Garg, S. / Sowers, T.S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    AIAA-2007-1323 A MODEL FOR PREDICTION OF CORNER SEPARATION

    Ji, L.-C. / Cheng, R. / Yi, W. et al. | British Library Conference Proceedings | 2007