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Results: 26-50/274
Authors:
STOLLERY J
Citation: J. Stollery, SPECIAL EDITIONS OF THE AERONAUTICAL-JOURNAL, Aeronautical Journal, 102(1012), 1998, pp. 61-61
Authors:
LOWSON M
Citation: M. Lowson, GOLDEN-JUBILEE OF THE DEPARTMENT-OF-AEROSPACE-ENGINEERING AT BRISTOL-UNIVERSITY, Aeronautical Journal, 102(1012), 1998, pp. 61-61
Authors:
HARDEN JM
LOWSON MV
Citation: Jm. Harden et Mv. Lowson, UNSTEADY PROPELLER FLOWS DUE TO TURBULENCE INGESTION, Aeronautical Journal, 102(1012), 1998, pp. 63-70
Authors:
GUHA A
Citation: A. Guha, COMPUTATION, ANALYSIS AND THEORY OF 2-PHASE FLOWS, Aeronautical Journal, 102(1012), 1998, pp. 71-82
Authors:
WISNOM MR
JONES MI
Citation: Mr. Wisnom et Mi. Jones, THROUGH-THICKNESS FATIGUE FAILURE OF FIBER-REINFORCED COMPOSITES, Aeronautical Journal, 102(1012), 1998, pp. 83-88
Authors:
GAITONDE AL
JONES DP
FIDDES SP
Citation: Al. Gaitonde et al., A 2D NAVIER-STOKES METHOD FOR UNSTEADY COMPRESSIBLE FLOW CALCULATIONSON MOVING MESHES, Aeronautical Journal, 102(1012), 1998, pp. 89-97
Authors:
JOHNSON DM
OMIECINSKI TA
Citation: Dm. Johnson et Ta. Omiecinski, THE FEASIBILITY AND BENEFITS OF DYNAMIC RECONFIGURATION IN INTEGRATEDMODULAR AVIONICS, Aeronautical Journal, 102(1012), 1998, pp. 99-105
Authors:
POTTER KD
WISNOM MR
LOWSON MV
ADAMS RD
Citation: Kd. Potter et al., INNOVATIVE APPROACHES TO COMPOSITE STRUCTURES, Aeronautical Journal, 102(1012), 1998, pp. 107-111
Authors:
ROHLFS M
Citation: M. Rohlfs, IDENTIFICATION OF NONLINEAR DERIVATIVE MODELS FROM BO-105 FLIGHT TESTDATA, Aeronautical Journal, 102(1011), 1998, pp. 1-8
Authors:
BERNSTEIN L
Citation: L. Bernstein, ON THE EQUATIONS OF MOTION FOR AN AIRCRAFT WITH AN INTERNAL MOVING LOAD WHICH IS THEN DROPPED, Aeronautical Journal, 102(1011), 1998, pp. 9-24
Authors:
RAISINGHANI SC
GHOSH AK
KALRA PK
Citation: Sc. Raisinghani et al., 2 NEW TECHNIQUES FOR AIRCRAFT PARAMETER-ESTIMATION USING NEURAL NETWORKS, Aeronautical Journal, 102(1011), 1998, pp. 25-30
Authors:
ALEID L
PILIDIS P
Citation: L. Aleid et P. Pilidis, VARIABLE CYCLE JET ENGINES FOR A MACH-2.7 SUPERSONIC CIVIL TRANSPORT, Aeronautical Journal, 102(1011), 1998, pp. 31-36
Authors:
STALKER RJ
PAULL A
Citation: Rj. Stalker et A. Paull, EXPERIMENTS ON CRUISE PROPULSION WITH A HYDROGEN SCRAMJET, Aeronautical Journal, 102(1011), 1998, pp. 37-43
Authors:
PAN H
RENDER PM
Citation: H. Pan et Pm. Render, STUDIES INTO HAIL INGESTION OF TURBOFAN ENGINES USING A ROTATING FAN AND SPINNER ASSEMBLY, Aeronautical Journal, 102(1011), 1998, pp. 45-51
Authors:
DJENIDI L
ANTONIA RA
HUNDSEID J
KROGSTAD PA
Citation: L. Djenidi et al., COMBINED EFFECT OF WALL SUCTION AND RIBLETS ON A LOW R-THETA TURBULENT BOUNDARY-LAYER, Aeronautical Journal, 102(1011), 1998, pp. 53-57
Authors:
MCLEAN D
ZOUAOUI Z
Citation: D. Mclean et Z. Zouaoui, AN AIRBORNE WINDSHEAR DETECTION SYSTEM, Aeronautical Journal, 101(1010), 1997, pp. 447-456
Authors:
ABEYRATNE RIR
Citation: Rir. Abeyratne, INTERNATIONAL OBLIGATIONS AS REGARDS SAFETY IN INTERNATIONAL CIVIL-AVIATION, Aeronautical Journal, 101(1010), 1997, pp. 457-466
Authors:
KLOMP ED
Citation: Ed. Klomp, PERFORMANCE OF STRAIGHT-WALLED ANNULAR DIFFUSERS WITH SWIRLING FLOW, Aeronautical Journal, 101(1010), 1997, pp. 467-480
Authors:
JOHNSTON AE
HANCOCK PE
Citation: Ae. Johnston et Pe. Hancock, SOME ASPECTS OF CENTRIFUGAL FAN CHARACTERISTICS IN BLOWER WINDTUNNELS, Aeronautical Journal, 101(1010), 1997, pp. 481-485
Authors:
NARANG BS
HO J
Citation: Bs. Narang et J. Ho, TRANSONIC FLOW OVER WAVY WALLS - A NEW SOLUTION PROCEDURE COMPARED WITH EXPERIMENTS, Aeronautical Journal, 101(1010), 1997, pp. 487-493
Authors:
CHIU T
FRIEDMANN PP
Citation: T. Chiu et Pp. Friedmann, AN ANALYTICAL MODEL FOR ACSR APPROACH TO VIBRATION REDUCTION IN A HELICOPTER ROTOR-FLEXIBLE FUSELAGE SYSTEM, Aeronautical Journal, 101(1009), 1997, pp. 399-408
Authors:
RINOIE K
Citation: K. Rinoie, STUDIES OF VORTEX FLAPS FOR DIFFERENT SWEEPBACK ANGLE DELTA-WINGS, Aeronautical Journal, 101(1009), 1997, pp. 409-416
A NOTE ON THE POTENTIAL CONTRIBUTION OF WING-BODY INTERFERENCE DRAG TO THE TOTAL DRAG OF AN AIRCRAFT
Authors:
BERNSTEIN L
Citation: L. Bernstein, A NOTE ON THE POTENTIAL CONTRIBUTION OF WING-BODY INTERFERENCE DRAG TO THE TOTAL DRAG OF AN AIRCRAFT, Aeronautical Journal, 101(1009), 1997, pp. 417-420
Authors:
HOLST H
BOCK KW
LORENZMEYER W
OBERDIECK F
HERMES M
Citation: H. Holst et al., OPERATIONAL EXPERIENCE AND TEST-RESULTS IN THE ADAPTIVE TEST SECTION OF THE DLR TRANSONIC TUNNEL, Aeronautical Journal, 101(1009), 1997, pp. 421-428
Authors:
GIACCHETTO A
Citation: A. Giacchetto, ON THE USE OF LARGE-SCALE WINDTUNNEL MODELS, Aeronautical Journal, 101(1009), 1997, pp. 429-437