Noise Prediction Technology for CTOL Aircraft
Author: John P. Raney
Publisher:
Published: 1977
Total Pages: 24
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: John P. Raney
Publisher:
Published: 1977
Total Pages: 24
ISBN-13:
DOWNLOAD EBOOKAuthor: John P. Raney
Publisher:
Published: 1975
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKAuthor: Interagency Aircraft Noise Research Panel
Publisher:
Published: 1975
Total Pages: 236
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1978
Total Pages: 540
ISBN-13:
DOWNLOAD EBOOKAuthor: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
Published: 2019-01-13
Total Pages: 32
ISBN-13: 9781793923035
DOWNLOAD EBOOKThe high fuel prices of recent years have caused the operating cost of the airlines to soar. In an effort to bring down the fuel consumption, the major aircraft engine manufacturers are now taking a fresh look at open rotors for the propulsion of future airliners. Open rotors, also known as propfans or unducted fans, can offer up to 30 per cent improvement in efficiency compared to high bypass engines of 1980 vintage currently in use in most civilian aircraft. NASA Langley researchers have contributed significantly to the development of aeroacoustic technology of open rotors. This report discusses the current noise prediction technology at Langley and reviews the input data requirements, strengths and limitations of each method as well as the associated problems in need of attention by the researchers. We present a brief history of research on the aeroacoustics of rotating blade machinery at Langley Research Center. We then discuss the available noise prediction codes for open rotors developed at NASA Langley and their capabilities. In particular, we present the two useful formulations used for the computation of noise from subsonic and supersonic surfaces. Here we discuss the open rotor noise prediction codes ASSPIN and one based on Ffowcs Williams-Hawkings equation with penetrable data surface (FW - Hpds). The scattering of sound from surfaces near the rotor are calculated using the fast scattering code (FSC) which is also discussed in this report. Plans for further improvements of these codes are given. Farassat, Fereidoun Langley Research Center WBS:561581.02.08.07.18.03
Author:
Publisher:
Published: 1978
Total Pages: 432
ISBN-13:
DOWNLOAD EBOOKAuthor: A-21 Aircraft Noise Measurement Aviation Emission Modeling
Publisher:
Published: 2012
Total Pages: 0
ISBN-13:
DOWNLOAD EBOOKThis document has been determined to contain basic and stable technology which is not dynamic in nature.
Author:
Publisher:
Published: 1977
Total Pages: 1092
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1978
Total Pages: 258
ISBN-13:
DOWNLOAD EBOOKAuthor: Evangelina Maria Thoma
Publisher:
Published: 2024
Total Pages: 0
ISBN-13: 9789181030143
DOWNLOAD EBOOK