Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise/

Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Division, Lewis Research Center
Format: Book
Language:English
Published: Washington: NASA, 1991
Series:NASA contractor report NASA CR-4329-4333
Subjects:
LEADER 01311nam a2200205 a 4500
001 702193
005 20171111231042.0
008 050510s1991 gr r f000 0 eng d
040 |a GR-KoDPT  |b gre  |e AACR2 
245 0 0 |a Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise/  |c D.B. Hanson 
260 |a Washington:  |b NASA,  |c 1991 
300 |a 5 τ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA contractor report  |v NASA CR-4329-4333 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
505 0 |a τ. 1. Development of theory for blade loading, wakes, and noise -- τ. 2. Development of theory for wing shielding / R.K. Amiet -- τ. 3. Application of theory for blade loading, wakes, noise and wing shielding / D.B. Hanson .. [et al.] -- τ. 4. Computer user's manual for UAAP turboprop aeroacoustic code / R.W. Menthe, C.J. McColgan, R.M. Ladden -- τ. 5. Propagation of propeller tone noise through a fuselage boundary layer / B. Magliozzi, D.B. Hanson 
650 0 |a Airplanes  |x Turbo-propeller engines  |x Noise 
650 0 |a Aerodynamics 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Division 
710 2 |a Lewis Research Center 
952 |a GR-KoDPT  |b 59cc20c46c5ad13446f88f8b  |c 998a  |d 945l  |e TL 521 .3  |t 1  |x m  |z Books