AAAAAA
Results: 1-25/274
Authors:
OWEN M
GALEA ER
LAWRENCE PJ
FILIPPIDIS L
Citation: M. Owen et al., THE NUMERICAL-SIMULATION OF AIRCRAFT EVACUATION AND ITS APPLICATION TO AIRCRAFT DESIGN AND CERTIFICATION, Aeronautical Journal, 102(1016), 1998, pp. 301-312
Authors:
BARRETT RV
SWALES C
Citation: Rv. Barrett et C. Swales, REALIZATION OF THE FULL-POTENTIAL OF THE LASER-DOPPLER ANEMOMETER IN THE ANALYSIS OF COMPLEX FLOWS, Aeronautical Journal, 102(1016), 1998, pp. 313-320
Authors:
RATCLIFFE MJ
LIEVEN NAJ
Citation: Mj. Ratcliffe et Naj. Lieven, AN IMPROVED METHOD FOR PARAMETER SELECTION IN FINITE-ELEMENT MODEL UPDATING, Aeronautical Journal, 102(1016), 1998, pp. 321-329
Authors:
ELLENRIEDER TJ
BRINSON PR
Citation: Tj. Ellenrieder et Pr. Brinson, THE DYNAMIC INDUCED VELOCITY-FIELD OF A MODEL ROTOR IN HOVER CONDITIONS, Aeronautical Journal, 102(1016), 1998, pp. 331-335
Authors:
GRANASY P
SORENSEN CB
MOSEKILDE E
THOMASSON PG
Citation: P. Granasy et al., NONLINEAR FLIGHT DYNAMICS AT HIGH ANGLES-OF-ATTACK, Aeronautical Journal, 102(1016), 1998, pp. 337-343
Authors:
YIP KM
LENG G
Citation: Km. Yip et G. Leng, STABILITY ANALYSIS FOR INVERSE SIMULATION OF AIRCRAFT, Aeronautical Journal, 102(1016), 1998, pp. 345-351
Authors:
STOLLERY J
Citation: J. Stollery, SURVEY ARTICLES IN THE AERONAUTICAL-JOURNAL, Aeronautical Journal, 102(1015), 1998, pp. 3-3
Authors:
HARRIS CJ
BAILEY A
DODD TJ
Citation: Cj. Harris et al., MULTISENSOR DATA FUSION IN DEFENSE AND AEROSPACE, Aeronautical Journal, 102(1015), 1998, pp. 229-244
Authors:
KESSLER C
REICHERT G
Citation: C. Kessler et G. Reichert, ACTIVE CONTROL TO AUGMENT ROTOR LEAD-LAG DAMPING, Aeronautical Journal, 102(1015), 1998, pp. 245-258
Authors:
MCINNES CR
Citation: Cr. Mcinnes, SATELLITE ATTITUDE SLEW MANEUVERS USING INVERSE CONTROL, Aeronautical Journal, 102(1015), 1998, pp. 259-265
Authors:
ELANGOVAN S
RATHAKRISHNAN E
Citation: S. Elangovan et E. Rathakrishnan, EFFECT OF CUTOUTS ON UNDEREXPANDED RECTANGULAR JETS, Aeronautical Journal, 102(1015), 1998, pp. 267-275
Authors:
MORRIS WD
CHANG SW
Citation: Wd. Morris et Sw. Chang, HEAT-TRANSFER IN A RADIALLY ROTATING SMOOTH-WALLED TUBE, Aeronautical Journal, 102(1015), 1998, pp. 277-285
Authors:
LANGLEY RS
BARDELL NS
Citation: Rs. Langley et Ns. Bardell, A REVIEW OF CURRENT ANALYSIS CAPABILITIES APPLICABLE TO THE HIGH-FREQUENCY VIBRATION PREDICTION OF AEROSPACE STRUCTURES, Aeronautical Journal, 102(1015), 1998, pp. 287-297
Authors:
JUPP JA
PRICE HJ
Citation: Ja. Jupp et Hj. Price, TRANSPORT AIRCRAFT - A CHALLENGE FOR ALUMINUM-ALLOYS FOR THE 21ST-CENTURY, Aeronautical Journal, 102(1014), 1998, pp. 181-188
Authors:
HOLMES JW
Citation: Jw. Holmes, ANALYSIS OF RADIOMETRIC, LIFETIME AND FLUORESCENT LIFETIME IMAGING FOR PRESSURE-SENSITIVE PAINT, Aeronautical Journal, 102(1014), 1998, pp. 189-194
Authors:
KOZIC MS
SREDOJEVIC D
Citation: Ms. Kozic et D. Sredojevic, DEVELOPMENT OF UNSTRUCTURED DYNAMIC GRIDS FOR SOLVING UNSTEADY 2-DIMENSIONAL EULER EQUATIONS, Aeronautical Journal, 102(1014), 1998, pp. 195-200
Authors:
HURST D
GALBRAITH RAM
COTON FN
GRANT I
Citation: D. Hurst et al., A FACILITY FOR SIMULTANEOUS PARTICLE IMAGE VELOCIMETRY AND HIGH-RESOLUTION UNSTEADY PRESSURE MEASUREMENT, Aeronautical Journal, 102(1014), 1998, pp. 201-209
Authors:
GENNARETTI M
CALCAGNO G
ZAMBONI A
MORINO L
Citation: M. Gennaretti et al., A HIGH-ORDER BOUNDARY-ELEMENT FORMULATION FOR POTENTIAL INCOMPRESSIBLE AERODYNAMICS, Aeronautical Journal, 102(1014), 1998, pp. 211-219
Authors:
RAFFEL M
SEELHORST U
WILLERT C
Citation: M. Raffel et al., VORTICAL FLOW STRUCTURES AT A HELICOPTER ROTOR MODEL MEASURED BY LDV AND PIV, Aeronautical Journal, 102(1014), 1998, pp. 221-227
Authors:
WILBY PG
Citation: Pg. Wilby, SHOCKWAVES IN THE ROTOR WORLD - A PERSONAL PERSPECTIVE OF 30 YEARS OFROTOR AERODYNAMIC DEVELOPMENTS IN THE UK, Aeronautical Journal, 102(1013), 1998, pp. 113-128
Authors:
ZHANG X
RONA A
EDWARDS JA
Citation: X. Zhang et al., THE EFFECT OF TRAILING-EDGE GEOMETRY ON CAVITY FLOW OSCILLATION DRIVEN BY A SUPERSONIC SHEAR-LAYER, Aeronautical Journal, 102(1013), 1998, pp. 129-136
Authors:
ANASTASIADIS PT
MORRIS AJ
HORNLEIN HREM
KRAMMER J
Citation: Pt. Anastasiadis et al., THE INFLUENCES ON OPTIMAL STRUCTURAL DESIGNS OF THE MODELING PROCESSES AND DESIGN CONCEPTS - PART-II - ALL COMPOSITE, RIB WING DESIGN CONCEPTS, Aeronautical Journal, 102(1013), 1998, pp. 137-150
Authors:
GAUTREY JE
COOK MV
Citation: Je. Gautrey et Mv. Cook, A GENERIC CONTROL ANTICIPATION PARAMETER FOR AIRCRAFT HANDLING QUALITIES EVALUATION, Aeronautical Journal, 102(1013), 1998, pp. 151-159
Authors:
HWANG DS
HSU PL
Citation: Ds. Hwang et Pl. Hsu, A ROBUST CONTROLLER-DESIGN FOR SUPERSONIC INTERMITTENT BLOWDOWN-TYPE WINDTUNNELS, Aeronautical Journal, 102(1013), 1998, pp. 161-169
Authors:
BARBEROPOULOS AA
GARRY KP
Citation: Aa. Barberopoulos et Kp. Garry, THE EFFECT OF SKEWING ON THE VORTICITY PRODUCED BY AN AIRJET VORTEX GENERATOR, Aeronautical Journal, 102(1013), 1998, pp. 171-177