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Results: 1-9 |
Results: 9
STRUCTURAL OPTIMIZATION FOR VIBRATORY LOADS REDUCTION OF COMPOSITE HELICOPTER ROTOR BLADES WITH ADVANCED GEOMETRY TIPS
Authors: YUAN KA FRIEDMANN PP
Citation: Ka. Yuan et Pp. Friedmann, STRUCTURAL OPTIMIZATION FOR VIBRATORY LOADS REDUCTION OF COMPOSITE HELICOPTER ROTOR BLADES WITH ADVANCED GEOMETRY TIPS, Journal of the American Helicopter Society, 43(3), 1998, pp. 246-256
CORRELATION STUDIES FOR HINGELESS ROTORS IN FORWARD FLIGHT USING 2GCHAS
Authors: MILLOTT TA FRIEDMANN PP YUAN KA
Citation: Ta. Millott et al., CORRELATION STUDIES FOR HINGELESS ROTORS IN FORWARD FLIGHT USING 2GCHAS, Journal of the American Helicopter Society, 43(3), 1998, pp. 257-262
ADAPTIVE-CONTROL OF AEROELASTIC INSTABILITIES IN TRANSONIC FLOW AND ITS SCALING
Authors: FRIEDMANN PP GUILLOT D PRESENTE E
Citation: Pp. Friedmann et al., ADAPTIVE-CONTROL OF AEROELASTIC INSTABILITIES IN TRANSONIC FLOW AND ITS SCALING, Journal of guidance, control, and dynamics, 20(6), 1997, pp. 1190-1199
AN ANALYTICAL MODEL FOR ACSR APPROACH TO VIBRATION REDUCTION IN A HELICOPTER ROTOR-FLEXIBLE FUSELAGE SYSTEM
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
VIBRATION REDUCTION IN ROTORCRAFT USING ACTIVE CONTROL - A COMPARISONOF VARIOUS APPROACHES
Authors: FRIEDMANN PP MILLOTT TA
Citation: Pp. Friedmann et Ta. Millott, VIBRATION REDUCTION IN ROTORCRAFT USING ACTIVE CONTROL - A COMPARISONOF VARIOUS APPROACHES, Journal of guidance, control, and dynamics, 18(4), 1995, pp. 664-673
FREE AND FORCED RESPONSE OF MULTISPAN BEAMS AND MULTI-BAY TRUSSES WITH LOCALIZED MODES
Authors: LUST SD FRIEDMANN PP BENDIKSEN OO
Citation: Sd. Lust et al., FREE AND FORCED RESPONSE OF MULTISPAN BEAMS AND MULTI-BAY TRUSSES WITH LOCALIZED MODES, Journal of sound and vibration, 180(2), 1995, pp. 313-332
A NEW SENSITIVITY ANALYSIS FOR STRUCTURAL OPTIMIZATION OF COMPOSITE ROTOR BLADES
Authors: VENKATESAN C FRIEDMANN PP YUAN KA
Citation: C. Venkatesan et al., A NEW SENSITIVITY ANALYSIS FOR STRUCTURAL OPTIMIZATION OF COMPOSITE ROTOR BLADES, Mathematical and computer modelling, 19(3-4), 1994, pp. 1-25
COUPLED ROTOR-FUSELAGE VIBRATION REDUCTION USING OPEN-LOOP BLADE PITCH CONTROL
Authors: PAPAVASSILIOU I FRIEDMANN PP VENKATESAN C
Citation: I. Papavassiliou et al., COUPLED ROTOR-FUSELAGE VIBRATION REDUCTION USING OPEN-LOOP BLADE PITCH CONTROL, Mathematical and computer modelling, 18(3-4), 1993, pp. 131-156
INTEGRATED STRUCTURE CONTROL AERODYNAMIC SYNTHESIS OF ACTIVELY CONTROLLED COMPOSITE WINGS
Authors: LIVNE E SCHMIT LA FRIEDMANN PP
Citation: E. Livne et al., INTEGRATED STRUCTURE CONTROL AERODYNAMIC SYNTHESIS OF ACTIVELY CONTROLLED COMPOSITE WINGS, Journal of aircraft, 30(3), 1993, pp. 387-394
Risultati: 1-9 |