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A Comparison of Combustor-Noise Models
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (08/06/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
The current status of combustor-noise prediction in the NASA Aircraft Noise Prediction Program (ANOPP) for current-generation (N) turbofan engines is summarized. Best methods for near-term updates are reviewed. Long-term needs and challenges for the N+1 through N+3 timeframe are discussed. This work was carried out under the NASA Fundamental Aeronautics Program, Subsonic Fixed Wing Project, Quiet Aircraft Subproject. Hultgren, Lennart, S. Glenn Research Center NASA/TM-2012-217671, AIAA Paper- 2012-2087, E-18346 WBS 561581.02.08.03.45.02.01 TURBOFAN ENGINES; NOISE PREDICTION; AEROACOUSTICS; AIRCRAFT CONFIGURATIONS; COMBUSTION CHAMBERS; FIXED WINGS
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Product Details
ISBN-13:
9798672796338
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
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Page Count:
34
Carton Quantity:
120
Product Dimensions:
8.50 x 0.07 x 11.02 inches
Weight:
0.23 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
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The current status of combustor-noise prediction in the NASA Aircraft Noise Prediction Program (ANOPP) for current-generation (N) turbofan engines is summarized. Best methods for near-term updates are reviewed. Long-term needs and challenges for the N+1 through N+3 timeframe are discussed. This work was carried out under the NASA Fundamental Aeronautics Program, Subsonic Fixed Wing Project, Quiet Aircraft Subproject. Hultgren, Lennart, S. Glenn Research Center NASA/TM-2012-217671, AIAA Paper- 2012-2087, E-18346 WBS 561581.02.08.03.45.02.01 TURBOFAN ENGINES; NOISE PREDICTION; AEROACOUSTICS; AIRCRAFT CONFIGURATIONS; COMBUSTION CHAMBERS; FIXED WINGS
Show More