Report discusses use of coupled aerodynamic/ and acoustical computer codes to predict noise emitted by turbopropeller blades turning at supersonic tip speeds. To predict noise field, existing turboprop-noise computer code by Farassat modified to accept blade-pressure inputs from three-dimensional turbofan aerodynamical computer code by Denton.
Coupled Aerodynamic/Acoustical Predictions For Turboprops
NASA Tech Briefs ; 12 , 5
01.05.1988
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1955
|British Library Online Contents | 2001
Online Contents | 1996
Pistons/Non-Pressurized Turboprops
British Library Online Contents | 2001
Online Contents | 1995
|