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The Effect of Bypass Nozzle Exit Area on Fan Aerodynamic Performance and Noise in a Model Turbofan Simulator
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (08/07/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
Technical Report Hughes, Christopher E. and Podboy, Gary, G. and Woodward, Richard P. and Jeracki, Robert, J. Glenn Research Center NASA/TM-2013-214029, GT2005-68573, E-15384 WBS 22-781-30-75 NOISE REDUCTION; TURBOFAN ENGINES; AEROACOUSTICS; AERODYNAMIC NOISE; FAN BLADES; AERODYNAMIC CHARACTERISTICS; FAR FIELDS; NOZZLE FLOW; AIRCRAFT NOISE; LOW SPEED WIND TUNNELS; LASER DOPPLER VELOCIMETERS; SCALE MODELS
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Product Format
Product Details
ISBN-13:
9798673171509
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
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Page Count:
42
Carton Quantity:
97
Product Dimensions:
8.50 x 0.09 x 11.02 inches
Weight:
0.27 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
Technical Report Hughes, Christopher E. and Podboy, Gary, G. and Woodward, Richard P. and Jeracki, Robert, J. Glenn Research Center NASA/TM-2013-214029, GT2005-68573, E-15384 WBS 22-781-30-75 NOISE REDUCTION; TURBOFAN ENGINES; AEROACOUSTICS; AERODYNAMIC NOISE; FAN BLADES; AERODYNAMIC CHARACTERISTICS; FAR FIELDS; NOZZLE FLOW; AIRCRAFT NOISE; LOW SPEED WIND TUNNELS; LASER DOPPLER VELOCIMETERS; SCALE MODELS
Show More