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Results: 1-6 |
Results: 6

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

Authors: VLAHOPOULOS N LYLE KH BURLEY CL
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

Authors: KITAPLIOGLU C CARADONNA FX BURLEY CL
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

Authors: BRENTNER KS BURLEY CL MARCOLINI MA
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
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