Citation: Dh. Hodges et al., FINITE-ELEMENT SOLUTION OF NONLINEAR INTRINSIC EQUATIONS FOR CURVED COMPOSITE BEAMS, Journal of the American Helicopter Society, 41(4), 1996, pp. 313-321
Citation: Jd. Keller, AN INVESTIGATION OF HELICOPTER DYNAMIC COUPLING USING AN ANALYTICAL MODEL, Journal of the American Helicopter Society, 41(4), 1996, pp. 322-330
Citation: Dh. Sweet, DEVELOPMENT OF THE S-76B PT6B-36B ENGINE ACCELERATION SCHEDULE/, Journal of the American Helicopter Society, 41(4), 1996, pp. 331-341
Citation: Jg. Leishman et al., MEASUREMENTS OF ROTOR TIP VORTICES USING 3-COMPONENT LASER-DOPPLER VELOCIMETRY, Journal of the American Helicopter Society, 41(4), 1996, pp. 342-353
Citation: Je. Stewart, 2 ALTERNATIVE VELOCITY VECTOR CUES FOR THE AH-64D - A COMPARATIVE-EVALUATION, Journal of the American Helicopter Society, 41(4), 1996, pp. 354-359
Citation: Tr. Mccarthy et A. Chattopadhyay, A COUPLED ROTOR WING OPTIMIZATION PROCEDURE FOR HIGH-SPEED TILT-ROTORAIRCRAFT/, Journal of the American Helicopter Society, 41(4), 1996, pp. 360-369
Authors:
SUBRAMANIAN S
GAONKAR GH
NAGABHUSHANAM J
NAKADI RM
Citation: S. Subramanian et al., PARALLEL COMPUTING CONCEPTS AND METHODS FOR FLOQUET ANALYSIS OF HELICOPTER TRIM AND STABILITY, Journal of the American Helicopter Society, 41(4), 1996, pp. 370-382
Citation: Sr. Turnour et R. Celi, MODELING OF FLEXIBLE ROTOR BLADES FOR HELICOPTER FLIGHT DYNAMICS APPLICATIONS (VOL 41, PG 52, 1996), Journal of the American Helicopter Society, 41(3), 1996, pp. 191-193
Citation: Mb. Tischler et al., THE NEW ADS-33 PROCESS - CAUTIONS FOR IMPLEMENTATION - COMMENT, Journal of the American Helicopter Society, 41(3), 1996, pp. 194-195
Citation: A. Bagai et Jg. Leishman, FREE-WAKE ANALYSIS OF TANDEM, TILT-ROTOR AND COAXIAL ROTOR CONFIGURATIONS, Journal of the American Helicopter Society, 41(3), 1996, pp. 196-207
Citation: A. Rosen et A. Isser, THE INFLUENCE OF UNSTEADY AERODYNAMIC EFFECTS ON THE COUPLED FREE-VIBRATIONS OF ROTOR FLAPPING AND BODY PITCH AND ROLL IN HOVER, Journal of the American Helicopter Society, 41(3), 1996, pp. 208-218
Citation: Yy. Dang et al., PARALLEL METHODS FOR TURBULENCE SIMULATION AND HELICOPTER-RESPONSE PREDICTION, Journal of the American Helicopter Society, 41(3), 1996, pp. 219-231
Citation: Jh. Ruddy et Aj. Vizzini, BONDED REPAIR OF MINIMUM-GAUGE COMPOSITE SANDWICH STRUCTURES, Journal of the American Helicopter Society, 41(3), 1996, pp. 232-238
Citation: Dc. Fleming et Aj. Vizzini, OFF-AXIS ENERGY-ABSORPTION CHARACTERIZATION OF COMPOSITES FOR CRASHWORTHY ROTORCRAFT DESIGN, Journal of the American Helicopter Society, 41(3), 1996, pp. 239-246
Authors:
SMITH EC
GOVINDSWAMY K
BEALE MR
LESIEUTRE GA
Citation: Ec. Smith et al., FORMULATION, VALIDATION, AND APPLICATION OF A FINITE-ELEMENT MODEL FOR ELASTOMERIC LAG DAMPERS, Journal of the American Helicopter Society, 41(3), 1996, pp. 247-256
Authors:
SMITH EC
GOVINDSWAMY K
BEALE MR
VASCSINEC M
LESIEUTRE GA
Citation: Ec. Smith et al., AEROELASTIC RESPONSE AND STABILITY OF HELICOPTERS WITH ELASTOMERIC LAG DAMPERS, Journal of the American Helicopter Society, 41(3), 1996, pp. 257-266
Citation: F. Gandhi et I. Chopra, ANALYSIS OF BEARINGLESS MAIN ROTOR AEROELASTICITY USING AN IMPROVED TIME-DOMAIN NONLINEAR ELASTOMERIC DAMPER MODEL, Journal of the American Helicopter Society, 41(3), 1996, pp. 267-277
Citation: B. Lovera, AGUSTA - 40 YEARS IN THE HELICOPTER INDUSTRY - THE 15TH ALEXANDER-A-NIKOLSKY-LECTURE, Journal of the American Helicopter Society, 41(2), 1996, pp. 3-16
Citation: J. Prieur et al., AERODYNAMIC AND ACOUSTIC CALCULATIONS OF TRANSONIC NONLIFTING HOVERING ROTORS, Journal of the American Helicopter Society, 41(2), 1996, pp. 17-26
Citation: M. Mosher et Js. Light, STUDY OF NOISE ON A SMALL-SCALE HOVERING TILT ROTOR, Journal of the American Helicopter Society, 41(2), 1996, pp. 27-36
Citation: Sr. Gibbard et Ld. Reid, AN INVESTIGATION OF PRIMARY FLIGHT CONTROL FAILURE IN A PILOTED HELICOPTER, Journal of the American Helicopter Society, 41(2), 1996, pp. 37-43
Citation: Ja. Schroeder, EVALUATION OF SIMULATION MOTION FIDELITY CRITERIA IN THE VERTICAL ANDDIRECTIONAL AXES, Journal of the American Helicopter Society, 41(2), 1996, pp. 44-57
Citation: Aa. Hassan et al., A CONSISTENT APPROACH FOR MODELING THE AERODYNAMICS OF SELF-GENERATEDROTOR BLADE-VORTEX INTERACTIONS, Journal of the American Helicopter Society, 41(2), 1996, pp. 74-84
Citation: Wh. Weller, FUSELAGE STATE-FEEDBACK FOR AEROMECHANICAL STABILITY AUGMENTATION OF A BEARINGLESS MAIN ROTOR, Journal of the American Helicopter Society, 41(2), 1996, pp. 85-93