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Results: 1-25/82
Authors:
PETER J
Citation: J. Peter, NONLINEAR IMPLICIT SCHEME USING NEWTONS METHOD FOR THE NUMERICAL-SOLUTION OF THE NAVIER-STOKES EQUATIONS, Aerospace science and technology, 2(3), 1998, pp. 157-166
Authors:
LANGLOIS M
CASALIS G
ARNAL D
Citation: M. Langlois et al., ON THE PRACTICAL APPLICATION OF THE PSE APPROACH TO LINEAR-STABILITY ANALYSIS, Aerospace science and technology, 2(3), 1998, pp. 167-176
Authors:
KUBE R
SPLETTSTOESSER WR
WAGNER W
SEELHORST U
YU YH
TUNG C
BEAUMIER P
PRIEUR J
RAHIER G
SPIEGEL P
BOUTIER A
BROOKS TF
BURLEY CL
BOYD DD
MERCKER E
PENGEL K
Citation: R. Kube et al., HHC AEROACOUSTIC ROTOR TESTS IN THE GERMAN-DUTCH WIND-TUNNEL - IMPROVING PHYSICAL UNDERSTANDING AND PREDICTION CODES, Aerospace science and technology, 2(3), 1998, pp. 177-190
Authors:
MICHELASSI V
RODI W
GIESS PA
Citation: V. Michelassi et al., EXPERIMENTAL AND NUMERICAL INVESTIGATION OF BOUNDARY-LAYER AND WAKE DEVELOPMENT IN A TRANSONIC TURBINE CASCADE, Aerospace science and technology, 2(3), 1998, pp. 191-204
Authors:
CHANETZ B
BENAY R
BOUSQUET JM
BUR R
POT T
GRASSO F
MOSS J
Citation: B. Chanetz et al., EXPERIMENTAL AND NUMERICAL STUDY OF THE LAMINAR SEPARATION IN HYPERSONIC FLOW, Aerospace science and technology, 2(3), 1998, pp. 205-218
Authors:
NAVAZ HK
BERG RM
Citation: Hk. Navaz et Rm. Berg, NUMERICAL TREATMENT OF MULTIPHASE FLOW EQUATIONS WITH CHEMISTRY AND STIFF SOURCE TERMS, Aerospace science and technology, 2(3), 1998, pp. 219-229
Authors:
HENTSCHEL R
Citation: R. Hentschel, THE CREATION OF LIFT BY SHARP-EDGED DELTA-WINGS - AN ANALYSIS OF A SELF-ADAPTIVE NUMERICAL-SIMULATION USING THE CONCEPT OF VORTICITY CONTENT, Aerospace science and technology, 2(2), 1998, pp. 79-90
Authors:
GEROLYMOS GA
BREUS JP
Citation: Ga. Gerolymos et Jp. Breus, COMPUTATION OF UNSTEADY NOZZLE-FLOW RESULTING FROM FLUCTUATING BACK-PRESSURE USING EULER EQUATIONS, Aerospace science and technology, 2(2), 1998, pp. 91-105
Authors:
COELHO PJ
DUIC N
LEMOS C
CARVALHO MG
Citation: Pj. Coelho et al., MODELING OF A SOLID-FUEL COMBUSTION-CHAMBER OF A RAMJET USING A MULTIBLOCK DOMAIN DECOMPOSITION TECHNIQUE, Aerospace science and technology, 2(2), 1998, pp. 107-119
Authors:
COCCIOLI R
PELOSI G
RAVANELLI R
Citation: R. Coccioli et al., A MODE MATCHING INTEGRAL-EQUATION TECHNIQUE FOR THE ANALYSIS AND DESIGN OF CORRUGATED HORNS, Aerospace science and technology, 2(2), 1998, pp. 121-128
Authors:
RIEDEL H
RONZHEIMER A
SITZMANN M
Citation: H. Riedel et al., ANALYSIS OF THE STATIC PRESSURE DISTRIBUTION ON A LAMINAR-FLOW NACELLE BASED ON EULER CALCULATIONS AND FLIGHT MEASUREMENTS, Aerospace science and technology, 2(2), 1998, pp. 129-143
Authors:
DELFS J
HELLER H
Citation: J. Delfs et H. Heller, AEROACOUSTICS RESEARCH IN EUROPE - 1996 HIGHLIGHTS, Aerospace science and technology, 2(2), 1998, pp. 145-154
Authors:
RIEDEL H
HORSTMANN KH
RONZHEIMER A
SITZMANN M
Citation: H. Riedel et al., AERODYNAMIC DESIGN OF A NATURAL LAMINAR-FLOW NACELLE AND THE DESIGN VALIDATION BY FLIGHT TESTING, Aerospace science and technology, 2(1), 1998, pp. 1-12
Authors:
MINH DK
BASDEVANT C
HIEPLE T
DANGTRAN K
Citation: Dk. Minh et al., TOPOLOGICAL AND DYNAMICAL ANALYSIS OF A 3-DIMENSIONAL MIXING-LAYER, Aerospace science and technology, 2(1), 1998, pp. 13-26
Authors:
KOENIG K
MULLER G
GRAHLMANN U
Citation: K. Koenig et al., SOME REMARKS ON THE ACOUSTIC FATIGUE OF ALUMINUM SKIN-STRINGER STRUCTURES WITH EITHER INTEGRALLY MILLED OR RIVETTED EDGE REINFORCEMENTS, Aerospace science and technology, 2(1), 1998, pp. 27-36
Authors:
CASALIS G
ROBINET JC
Citation: G. Casalis et Jc. Robinet, LINEAR-STABILITY ANALYSIS IN TRANSONIC DIFFUSER FLOWS, Aerospace science and technology, 2(1), 1998, pp. 37-47
Authors:
SACHS G
Citation: G. Sachs, PATH-ATTITUDE DECOUPLING AND FLYING QUALITIES IMPLICATIONS IN HYPERSONIC FLIGHT, Aerospace science and technology, 2(1), 1998, pp. 49-59
Authors:
BUR R
DELERY J
CORBEL B
SOULEVANT D
SOARES R
Citation: R. Bur et al., A BASIC EXPERIMENTAL INVESTIGATION OF PASSIVE CONTROL APPLIED TO A TRANSONIC INTERACTION, Aerospace science and technology, 2(1), 1998, pp. 61-73
Authors:
GORDNIER RE
VISBAL MR
Citation: Re. Gordnier et Mr. Visbal, NUMERICAL-SIMULATION OF DELTA-WING ROLL, La Recherche aerospatiale, 2(6), 1998, pp. 347-357
Authors:
LO RE
Citation: Re. Lo, A NOVEL KIND OF SOLID ROCKET PROPELLANT, La Recherche aerospatiale, 2(6), 1998, pp. 359-367
Authors:
THIONNET A
RENARD J
Citation: A. Thionnet et J. Renard, EXPERIMENTAL AND NUMERICAL STUDY OF A FIBRE MATRIX INTERFACE OF SIC/TITANIUM COMPOSITES/, La Recherche aerospatiale, 2(6), 1998, pp. 369-379
Authors:
SCHUTZE R
GOETTING HC
BREITBACH E
GRUTZMACHER T
Citation: R. Schutze et al., LIGHTWEIGHT ENGINE MOUNTING BASED ON ADAPTIVE CFRP STRUTS FOR ACTIVE VIBRATION SUPPRESSION, La Recherche aerospatiale, 2(6), 1998, pp. 381-390
Authors:
WOLFINGER C
ARENDTS FJ
FRIEDRICH K
DRECHSLER K
Citation: C. Wolfinger et al., HEALTH-MONITORING-SYSTEM BASED ON PIEZOELECTRIC TRANSDUCERS, La Recherche aerospatiale, 2(6), 1998, pp. 391-400
Authors:
BASTIERE A
Citation: A. Bastiere, METHODS FOR MULTISENSOR CLASSIFICATION OF AIRBORNE TARGETS INTEGRATING EVIDENCE THEORY, La Recherche aerospatiale, 2(6), 1998, pp. 401-411
Authors:
BERDE B
BORREL M
Citation: B. Berde et M. Borrel, NUMERICAL EXPERIMENTS ON THE ACCURACY OF A DISCONTINUOUS GALERKIN METHOD FOR THE EULER EQUATIONS, La Recherche aerospatiale, 2(5), 1998, pp. 279-288