Authors:
SCHULTZ KJ
SPLETTSTOESSER W
JUNKER B
WAGNER W
ARNAUD G
SCHOELL E
FERTIS D
MERCKER E
PENGEL K
Citation: Kj. Schultz et al., A PARAMETRIC WINDTUNNEL TEST ON ROTORCRAFT AERODYNAMICS AND AEROACOUSTICS (HELISHAPE) - TEST PROCEDURES AND REPRESENTATIVE RESULTS, Aeronautical Journal, 101(1004), 1997, pp. 143-154
Citation: G. Lombardi et G. Mengali, A METHODOLOGY FOR THE PRELIMINARY-ANALYSIS AND COMPARISON OF WING-TAIL AND CANARD CONFIGURATIONS, Aeronautical Journal, 101(1004), 1997, pp. 169-177
Citation: G. Guglieri et Fb. Quagliotti, EXPERIMENTAL INVESTIGATION OF VORTEX DYNAMICS ON A 65-DEGREES DELTA-WING IN SIDESLIP, Aeronautical Journal, 101(1003), 1997, pp. 111-120
Citation: Scm. Yu et Th. Yip, MEASUREMENTS OF VELOCITIES IN THE NEAR-FIELD OF A LOBED FORCED MIXER TRAILING-EDGE, Aeronautical Journal, 101(1003), 1997, pp. 121-129
Citation: Kp. Sinhamahapatra et N. Singh, 2-DIMENSIONAL IMPLICIT FLUX SPLIT STEADY AND UNSTEADY EULER CALCULATIONS USING UNSTRUCTURED MOVING GRIDS, Aeronautical Journal, 101(1003), 1997, pp. 131-139
Authors:
YANG G
CAUSON DM
INGRAM DM
SAUNDERS R
BATTEN P
Citation: G. Yang et al., A CARTESIAN CUT CELL METHOD FOR COMPRESSIBLE FLOWS .A. STATIC BODY PROBLEMS, Aeronautical Journal, 101(1002), 1997, pp. 47-56
Authors:
YANG G
CAUSON DM
INGRAM DM
SAUNDERS R
BATTEN P
Citation: G. Yang et al., A CARTESIAN CUT CELL METHOD FOR COMPRESSIBLE FLOWS .B. MOVING BODY PROBLEMS, Aeronautical Journal, 101(1002), 1997, pp. 57-65
Citation: M. Lillico et al., AEROELASTIC OPTIMIZATION OF COMPOSITE WINGS USING THE DYNAMIC STIFFNESS METHOD, Aeronautical Journal, 101(1002), 1997, pp. 77-86
Citation: Lw. Traub, EFFECTS OF DELTA-PLANFORM TIP SAILS ON THE PERFORMANCE OF A BLUNT EDGED RECTANGULAR WING, Aeronautical Journal, 101(1002), 1997, pp. 87-92
Citation: Jc. Gibbings et Sm. Alshukri, EFFECT OF SANDPAPER ROUGHNESS AND STREAM TURBULENCE ON THE LAMINAR LAYER AND ITS TRANSITION, Aeronautical Journal, 101(1001), 1997, pp. 17-24
Citation: Sk. Morton et Jph. Webber, HEURISTIC DESIGN OF COMPOSITE LAMINATES FOR STRENGTH, STIFFNESS AND MULTIPLE LOAD CASES, Aeronautical Journal, 101(1001), 1997, pp. 35-45
Citation: N. Qin, INCIPIENT SEPARATION BOUNDARY - CONFIRMATION OF AN EMPIRICAL CRITERION BY NAVIER-STOKES SOLUTIONS, Aeronautical Journal, 100(999), 1996, pp. 381-384