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Results: 51-75/1034
Authors:
GREENMAN RM
CHEUNG S
TU EL
Citation: Rm. Greenman et al., COUPLED NAVIER-STOKES AND OPTIMIZER ANALYSIS OF A TRANSONIC WING, Journal of aircraft, 35(3), 1998, pp. 362-369
Authors:
WETZEL TG
SIMPSON RL
Citation: Tg. Wetzel et Rl. Simpson, EFFECTS OF FIN AND JET VORTEX GENERATORS ON THE CROSS-FLOW, Journal of aircraft, 35(3), 1998, pp. 370-379
Authors:
SANGHI V
KUMAR SK
SUNDARARAJAN V
SANE SK
Citation: V. Sanghi et al., ENGINE-AIRFRAME INTEGRATION DURING CONCEPTUAL DESIGN FOR MILITARY APPLICATION, Journal of aircraft, 35(3), 1998, pp. 380-386
Authors:
SCHWABACHER M
GELSEY A
Citation: M. Schwabacher et A. Gelsey, MULTILEVEL SIMULATION AND NUMERICAL OPTIMIZATION OF COMPLEX ENGINEERING DESIGNS, Journal of aircraft, 35(3), 1998, pp. 387-397
Authors:
GOPALARATHNAM A
SELIG MS
Citation: A. Gopalarathnam et Ms. Selig, MULTIPOINT INVERSE METHOD FOR MULTIELEMENT AIRFOIL DESIGN, Journal of aircraft, 35(3), 1998, pp. 398-404
Authors:
KORIVI VM
NEWMAN PA
TAYLOR AC
Citation: Vm. Korivi et al., AERODYNAMIC OPTIMIZATION USING SENSITIVITY DERIVATIVES FROM A 3-DIMENSIONAL SUPERSONIC EULER CODE, Journal of aircraft, 35(3), 1998, pp. 405-411
Authors:
HOLST TL
Citation: Tl. Holst, MULTIZONE CHIMERA ALGORITHM FOR SOLVING THE FULL-POTENTIAL EQUATION, Journal of aircraft, 35(3), 1998, pp. 412-421
Authors:
LIU HT
GOLBORNE C
BUN Y
BARTEL M
Citation: Ht. Liu et al., SURFACE WINDSHEAR ALERT SYSTEM, PART 1 - PROTOTYPE DEVELOPMENT, Journal of aircraft, 35(3), 1998, pp. 422-428
Authors:
LIU HT
Citation: Ht. Liu, SURFACE WINDSHEAR ALERT SYSTEM, PART 2 - FIELD-TESTS, Journal of aircraft, 35(3), 1998, pp. 429-436
Authors:
KARPEL M
Citation: M. Karpel, MODAL-BASED ENHANCEMENT OF INTEGRATED DESIGN OPTIMIZATION SCHEMES, Journal of aircraft, 35(3), 1998, pp. 437-444
Authors:
GEYER WP
SMITH EC
KELLER JA
Citation: Wp. Geyer et al., AEROELASTIC ANALYSIS OF TRANSIENT BLADE DYNAMICS DURING SHIPBOARD ENGAGE DISENGAGE OPERATIONS/, Journal of aircraft, 35(3), 1998, pp. 445-453
Authors:
GADE PVN
INMAN DJ
Citation: Pvn. Gade et Dj. Inman, ACTIVE CONTROL OF STORE-INDUCED FLUTTER IN INCOMPRESSIBLE-FLOW, Journal of aircraft, 35(3), 1998, pp. 454-461
Authors:
ANDRIGHETTONI M
MANTEGAZZA P
Citation: M. Andrighettoni et P. Mantegazza, MULTI-INPUT MULTI-OUTPUT ADAPTIVE ACTIVE FLUTTER SUPPRESSION FOR A WING MODEL/, Journal of aircraft, 35(3), 1998, pp. 462-469
Authors:
LIND R
BRENNER M
Citation: R. Lind et M. Brenner, INCORPORATING FLIGHT DATA INTO A ROBUST AEROELASTIC MODEL, Journal of aircraft, 35(3), 1998, pp. 470-477
Authors:
JAUNKY N
KNIGHT NF
AMBUR DR
Citation: N. Jaunky et al., OPTIMAL-DESIGN OF GRID-STIFFENED COMPOSITE PANELS USING GLOBAL AND LOCAL BUCKLING ANALYSES, Journal of aircraft, 35(3), 1998, pp. 478-486
Authors:
BELLINGER NC
KOMOROWSKI JP
GOULD RW
Citation: Nc. Bellinger et al., DAMAGE TOLERANCE IMPLICATIONS OF CORROSION PILLOWING ON FUSELAGE LAP JOINTS, Journal of aircraft, 35(3), 1998, pp. 487-491
Authors:
RUSSO GP
ZUPPARDI G
LUPO FM
Citation: Gp. Russo et al., SIMPLIFIED METHOD FOR TESTING FINITE WINGS IN WIND TUNNELS WITH 2 ADAPTIVE WALLS, Journal of aircraft, 35(3), 1998, pp. 492-494
Authors:
MATHIAS DL
STORMS BL
ROSS JC
Citation: Dl. Mathias et al., LIFT-ENHANCING TABS ON SWEPT, 3-DIMENSIONAL HIGH-LIFT SYSTEMS, Journal of aircraft, 35(3), 1998, pp. 494-495
Authors:
IZE C
ARENA AS
Citation: C. Ize et As. Arena, SPANWISE CAMBER AND QUASI-STEADY EFFECTS DURING WING ROCK, Journal of aircraft, 35(3), 1998, pp. 495-497
Authors:
NEWMAN RL
Citation: Rl. Newman, DEFINITION OF PRIMARY FLIGHT REFERENCE, Journal of aircraft, 35(3), 1998, pp. 497-500
Authors:
RAO MS
HASSAN HA
Citation: Ms. Rao et Ha. Hassan, MODELING TURBULENCE IN THE PRESENCE OF ADVERSE PRESSURE-GRADIENTS, Journal of aircraft, 35(3), 1998, pp. 500-502
Authors:
BISMARCKNASR MN
Citation: Mn. Bismarcknasr, BUCKLING ANALYSIS OF LAMINATED FIBER-REINFORCED DOUBLY-CURVED SHALLOWSHELLS, Journal of aircraft, 35(3), 1998, pp. 502-505
Authors:
KUTTENKEULER J
RINGERTZ U
Citation: J. Kuttenkeuler et U. Ringertz, AEROELASTIC DESIGN OPTIMIZATION WITH EXPERIMENTAL-VERIFICATION, Journal of aircraft, 35(3), 1998, pp. 505-507
Authors:
HSIAO FB
LIANG PF
HUANG CY
Citation: Fb. Hsiao et al., HIGH-INCIDENCE AIRFOIL AERODYNAMICS IMPROVEMENT BY LEADING-EDGE OSCILLATING FLAP, Journal of aircraft, 35(3), 1998, pp. 508-510
Authors:
NAVEH T
SEIFERT A
TUMIN A
WYGNANSKI I
Citation: T. Naveh et al., SWEEP EFFECT ON PARAMETERS GOVERNING CONTROL OF SEPARATION BY PERIODIC EXCITATION, Journal of aircraft, 35(3), 1998, pp. 510-512