Authors:
KUBE R
SPLETTSTOESSER WR
WAGNER W
SEELHORST U
YU YH
TUNG C
BEAUMIER P
PRIEUR J
RAHIER G
SPIEGEL P
BOUTIER A
BROOKS TF
BURLEY CL
BOYD DD
MERCKER E
PENGEL K
Citation: R. Kube et al., HHC AEROACOUSTIC ROTOR TESTS IN THE GERMAN-DUTCH WIND-TUNNEL - IMPROVING PHYSICAL UNDERSTANDING AND PREDICTION CODES, Aerospace science and technology, 2(3), 1998, pp. 177-190
Citation: N. Vlahopoulos et al., TECHNICAL NOTE - PRELIMINARY WORK FOR MODELING THE PROPELLERS OF AN AIRCRAFT AS A NOISE SOURCE IN AN ACOUSTIC BOUNDARY-ELEMENT ANALYSIS, Noise control engineering journal, 46(3), 1998, pp. 132-136
Authors:
GALLMAN JM
SCHULTZ KJ
SPIEGEL P
BURLEY CL
Citation: Jm. Gallman et al., EFFECT OF WAKE STRUCTURE ON BLADE-VORTEX INTERACTION PHENOMENA - ACOUSTIC PREDICTION AND VALIDATION, Journal of aircraft, 35(2), 1998, pp. 267-273
Citation: C. Kitaplioglu et al., PARALLEL BLADE-VORTEX INTERACTIONS - AN EXPERIMENTAL-STUDY AND COMPARISON WITH COMPUTATIONS, Journal of the American Helicopter Society, 42(3), 1997, pp. 272-281
Citation: Ks. Brentner et al., SENSITIVITY OF ACOUSTIC PREDICTIONS TO VARIATION OF INPUT PARAMETERS, Journal of the American Helicopter Society, 39(3), 1994, pp. 43-52
Authors:
VISINTAINER JA
MARCOLINI MA
BURLEY CL
LIU SR
Citation: Ja. Visintainer et al., ACOUSTIC PREDICTIONS USING MEASURED PRESSURES FROM A MODEL ROTOR IN THE DNW, Journal of the American Helicopter Society, 38(3), 1993, pp. 35-44