Citation: Fh. Schmitz, REDUCTION OF BLADE-VORTEX INTERACTION (BVI) NOISE THROUGH X-FORCE CONTROL, Journal of the American Helicopter Society, 43(1), 1998, pp. 14-24
Authors:
ARNOLD UTP
KELLER JD
CURTISS HC
REICHERT G
Citation: Utp. Arnold et al., THE EFFECT OF INFLOW MODELS ON THE PREDICTED RESPONSE OF HELICOPTERS, Journal of the American Helicopter Society, 43(1), 1998, pp. 25-36
Citation: E. Moedersheim et Jg. Leishman, INVESTIGATION OF AERODYNAMIC INTERACTIONS BETWEEN A ROTOR AND A T-TAIL EMPENNAGE, Journal of the American Helicopter Society, 43(1), 1998, pp. 37-46
Citation: Sr. Ahmed et Vt. Vidjaja, UNSTEADY PANEL METHOD CALCULATION OF PRESSURE DISTRIBUTION ON BO-105 MODEL ROTOR BLADES, Journal of the American Helicopter Society, 43(1), 1998, pp. 47-56
Authors:
LYRINTZIS AS
KOUTSAVDIS EK
BEREZIN CR
VISINTAINER JA
POLLACK MJ
Citation: As. Lyrintzis et al., AN EVALUATION OF A ROTATING KIRCHHOFF ACOUSTIC METHODOLOGY, Journal of the American Helicopter Society, 43(1), 1998, pp. 57-65
Citation: F. Gandhi et I. Chopra, AN AEROELASTIC ANALYSIS METHODOLOGY FOR BEARINGLESS MAIN ROTOR HELICOPTERS, Journal of the American Helicopter Society, 43(1), 1998, pp. 66-75
Citation: Re. Hansford et J. Vorwald, DYNAMICS WORKSHOP ON ROTOR VIBRATORY LOADS PREDICTION, Journal of the American Helicopter Society, 43(1), 1998, pp. 76-87
Citation: Dg. Thomson et R. Bradley, MATHEMATICAL DEFINITION OF HELICOPTER MANEUVERS, Journal of the American Helicopter Society, 42(4), 1997, pp. 307-309
Citation: Rg. Rajagopalan et Cn. Keys, DETAILED AERODYNAMIC ANALYSIS OF THE RAH-66 FANTAIL(TM) USING CFD, Journal of the American Helicopter Society, 42(4), 1997, pp. 310-320
Citation: P. Beaumier et al., CFD DRAG AND POWER PREDICTION FOR A ROTOR IN HOVER OR FORWARD FLIGHT - FORMULATION AND FIRST APPLICATIONS, Journal of the American Helicopter Society, 42(4), 1997, pp. 327-336
Citation: Yy. Dang et al., MODELING TURBULENCE SEEN BY MULTIBLADED ROTORS FOR PREDICTING ROTORCRAFT RESPONSE WITH 3-DIMENSIONAL WAKE, Journal of the American Helicopter Society, 42(4), 1997, pp. 337-349
Citation: Ja. Li et al., TEST AND ANALYSIS OF COMPOSITE HAT STRINGER PULL-OFF TEST SPECIMENS, Journal of the American Helicopter Society, 42(4), 1997, pp. 350-357
Citation: O. Song et L. Librescu, STRUCTURAL MODELING AND FREE-VIBRATION ANALYSIS OF ROTATING COMPOSITETHIN-WALLED-BEAMS, Journal of the American Helicopter Society, 42(4), 1997, pp. 358-369
Citation: Sj. Chunduru et al., DYNAMIC STALL AND WAKE EFFECTS ON TRIM AND STABILITY OF HINGELESS ROTORS WITH EXPERIMENTAL CORRELATION, Journal of the American Helicopter Society, 42(4), 1997, pp. 370-382
Citation: Ta. Ghee, INBOARD SHEET ROLL UP OF THE WAKE OF A SMALL-SCALE ROTOR SYSTEM, Journal of the American Helicopter Society, 42(4), 1997, pp. 383-386
Citation: B. Panda et E. Mychalowycz, AEROELASTIC STABILITY WIND-TUNNEL TESTING WITH ANALYTICAL CORRELATIONOF THE COMANCHE BEARINGLESS MAIN ROTOR, Journal of the American Helicopter Society, 42(3), 1997, pp. 207-217
Citation: R. Ganguli et I. Chopra, AEROELASTIC TAILORING OF COMPOSITE COUPLINGS AND BLADE GEOMETRY OF A HELICOPTER ROTOR USING OPTIMIZATION METHODS, Journal of the American Helicopter Society, 42(3), 1997, pp. 218-228
Citation: R. Guillemette, THE DEVELOPMENT AND IMPLEMENTATION OF THERMAL SPRAY COATINGS FOR HELICOPTER COMPONENTS, Journal of the American Helicopter Society, 42(3), 1997, pp. 229-234
Citation: Ms. Chaffin et Jd. Berry, HELICOPTER FUSELAGE AERODYNAMICS UNDER A ROTOR BY NAVIER-STOKES SIMULATION, Journal of the American Helicopter Society, 42(3), 1997, pp. 235-243
Citation: Ct. Jones et R. Celi, FREQUENCY-RESPONSE SENSITIVITY FUNCTIONS FOR HELICOPTER FREQUENCY-DOMAIN SYSTEM-IDENTIFICATION, Journal of the American Helicopter Society, 42(3), 1997, pp. 244-253
Citation: Mw. Heiges, RECONFIGURABLE CONTROLS FOR ROTORCRAFT - A FEASIBILITY STUDY, Journal of the American Helicopter Society, 42(3), 1997, pp. 254-263
Citation: W. Davis et al., EXTRACTING AND CHARACTERIZING BLADE-VORTEX INTERACTION NOISE WITH WAVELETS, Journal of the American Helicopter Society, 42(3), 1997, pp. 264-271