Effect of thrust vectoring on level-turn performance (English)
National licence
- New search for: LEE, PAI-HUNG
- New search for: LAN, C. E.
- New search for: LEE, PAI-HUNG
- New search for: LAN, C. E.
In:
Journal of Aircraft
;
29
, 3
;
509-511
;
1992
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ISSN:
- Article (Journal) / Electronic Resource
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Title:Effect of thrust vectoring on level-turn performance
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Contributors:LEE, PAI-HUNG ( author ) / LAN, C. E. ( author )
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Published in:Journal of Aircraft ; 29, 3 ; 509-511
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Publisher:
- New search for: The American Institute of Aeronautics and Astronautics
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Publication date:1992-01-01
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Size:3 pages
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ISSN:
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DOI:
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Type of media:Article (Journal)
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Type of material:Electronic Resource
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Language:English
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Source:
Table of contents – Volume 29, Issue 3
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 297
-
Subsonic and transonic low-Reynolds-number airfoils with reduced pitching momentsREUTHER, J. / VAN DAM / C. P. / HICKS, R. et al. | 1992
- 299
-
Analysis of airship lateral maneuverabilityNAGABHUSHAN, B. L. / PASHA, RAMIN P. K. et al. | 1992
- 301
-
Numerical simulation of leading-edge vortex breakdown using an EulercodeO'NEIL, P. J. / BARNETT, R. M. / LOUIE, C. M. et al. | 1992
- 308
-
Data analysis for unsteady turbulence measurements over airfoilsJOHNSON, DONALD K. / HOWARD, RICHARD M. / ILACQUA, PAUL N. et al. | 1992
- 314
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Design and development of a compressible dynamic stall facilityCARR, L. W. / NASA, Ames Research Center / Moffett Field / CA / CHANDRASEKHARA, M. S. et al. | 1992
- 319
-
Hazard evaluation and operational cockpit display of ground-measuredwindshear dataWANKE, CRAIG / HANSMAN, R. J. et al. | 1992
- 326
-
Transonic Navier-Stokes computations for an oscillating wing using zonal gridsCHADERJIAN, NEAL M. / GURUSWAMY, GURU P. et al. | 1992
- 336
-
Effects of higher harmonic control on rotor performance and control loadsNGUYEN, KHANH / CHOPRA, INDERJIT et al. | 1992
- 343
-
Design optimization of natural laminar flow bodies in compressible flowDODBELE, SIMHA S. et al. | 1992
- 348
-
Microwave landing system modeling with application to air traffic control automationPOULOSE, M. M. / NASA, Ames Research Center / Moffett Field / CA et al. | 1992
- 355
-
Software reliability for flight crew training simulatorsSTARK, GEORGE E. et al. | 1992
- 360
-
Control strategy for maximizing reconnaissance range of hypersonic cruise vehiclesKAUFFMAN, H. G. / GRANDHI, R. V. / HANKEY, W. L. / BELCHER, P. J. et al. | 1992
- 366
-
Unsteady aerodynamic loading produced by a sinusoidally oscillating delta wingHUYER, S. A. / ROBINSON, M. C. / LUTTGES, M. W. et al. | 1992
- 374
-
Extension and validation of an unsteady wake model for rotorsSU, AY / YOO, KYUNG M. / PETERS, DAVID A. et al. | 1992
- 384
-
Thermal management for a Mach 5 cruise aircraft using endothermic fuelPETLEY, DENNIS H. / JONES, STUART C. et al. | 1992
- 390
-
Identification of the transfer function between turbulence and aircraftCHEN, QING / SCHAENZER, GUNTHER et al. | 1992
- 396
-
Numerical study of vortex-dominated flows for wings at high incidence and sideslipHSU, C.-H. / LIU, C. H. et al. | 1992
- 404
-
Prediction of vortex shedding from forebodies with chinesMENDENHALL, MICHAEL R. / LESIEUTRE, DANIEL J. et al. | 1992
- 413
-
Flow over a twin-tailed aircraft at angle of attack. I - Spatial characteristicsKOMERATH, N. M. / LIOU, S. G. / SCHWARTZ, R. J. / KIM, J. M. et al. | 1992
- 421
-
Robust flight reconstruction for helicopter simulation and trainingKRISHNAKUMAR, K. / PRASANTH, R. K. / BAILEY, J. E. et al. | 1992
- 429
-
Drag reduction of bluff bodies through momentum injectionMODI, V. J. / SHIH, E. / YING, B. / YOKOMIZO, T. et al. | 1992
- 437
-
Wake effects on the prediction of transonic viscous flows around airfoilsCOIRO, D. P. / DE MATTEIS / P. / AMATO, M. et al. | 1992
- 444
-
Application of Active Flexible Wing technology to the Agile FalconPENDLETON, EDMUND / LEE, MARK / WASSERMAN, LEE et al. | 1992
- 452
-
Fighter agility metrics, research and testLIEFER, RANDALL K. / VALASEK, JOHN / EGGOLD, DAVID P. / DOWNING, DAVID R. et al. | 1992
- 458
-
Downwash for joined-wing airframe with control surface deflectionsBURKHALTER, JOHN E. / SPRING, DONALD J. / KEY, M. K. et al. | 1992
- 465
-
Improved measurement of the dynamic loads acting on rotating parachutesSHPUND, Z. / LEVIN, D. et al. | 1992
- 470
-
Composite material repairs to metallic airframe componentsCHRISTIAN, T. F. / HAMMOND, D. O. / COCHRAN, J. B. et al. | 1992
- 477
-
Transonic aeroelasticity analysis for rotor bladesGEA, LIE-MINE / CHOW, CHUEN-YEN / CHANG,I-CHUNG et al. | 1992
- 485
-
Thermal structures - Four decades of progressTHORNTON, EARL A. et al. | 1992
- 499
-
Structure-borne noise transmission in the Propfan Test Assessment aircraftUNRUH, JAMES F. et al. | 1992
- 505
-
Coalescence of aeroelastic modes in flutter analysisBISMARCK-NASR, MAHER N. et al. | 1992
- 507
-
Structural and aerodynamic data transformation using inverse isoparametric mappingPIDAPARTI, R. M. V. et al. | 1992
- 509
-
Effect of thrust vectoring on level-turn performanceLEE, PAI-HUNG / LAN, C. E. et al. | 1992
- 511
-
Transition of the flutter mode of a two-dimensional section with an external storeYANG, ZHI-CHUN / ZHAO, LING-CHENG et al. | 1992
- 513
-
Characteristic differences between the modal parameters of cast and forged structuresPANOSSIAN, H. V. et al. | 1992
- 516
-
Accurate prediction of drag using Euler methodsVAN DAM / C. P. / NIKFETRAT, K. et al. | 1992
- 519
-
Comment on 'Transition effects on airfoil dynamics and implications for subscale tests'MABEY, D. G. / ASHILL, P. R. et al. | 1992
- 520
-
Reply by Author to D. G. Mabey and P. R. AshillL. E. Ericsson et al. | 1992