ISBN 9781723842313 is currently unpriced. Please contact us for pricing.
Available options are listed below:
Available options are listed below:
Flow Solution for Advanced Separate Flow Nozzles Response a: Structured Grid Navier-Stokes Approach
| AUTHOR | Nasa, National Aeronautics and Space Adm |
| PUBLISHER | Independently Published (09/19/2018) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
NASA Glenn Research Center funded a computational study to investigate the effect of chevrons and tabs on the exhaust plume from separate flow nozzles. Numerical studies were conducted at typical takeoff power with 0.28 M flight speed. Report provides numerical data and insights into the mechanisms responsible for increased mixing.Kenzakowski, D. C. and Shipman, J. and Dash, S. M. and Saiyed, Naseem (Technical Monitor)Glenn Research CenterPLUMES; EXHAUST GASES; ACOUSTIC NOZZLES; STRUCTURED GRIDS (MATHEMATICS); AEROACOUSTICS; AIRCRAFT NOISE; MIXERS; NOISE REDUCTION...
Show More
Product Format
Product Details
ISBN-13:
9781723842313
ISBN-10:
1723842311
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
68
Carton Quantity:
60
Product Dimensions:
8.50 x 0.14 x 11.02 inches
Weight:
0.40 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Science | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
NASA Glenn Research Center funded a computational study to investigate the effect of chevrons and tabs on the exhaust plume from separate flow nozzles. Numerical studies were conducted at typical takeoff power with 0.28 M flight speed. Report provides numerical data and insights into the mechanisms responsible for increased mixing.Kenzakowski, D. C. and Shipman, J. and Dash, S. M. and Saiyed, Naseem (Technical Monitor)Glenn Research CenterPLUMES; EXHAUST GASES; ACOUSTIC NOZZLES; STRUCTURED GRIDS (MATHEMATICS); AEROACOUSTICS; AIRCRAFT NOISE; MIXERS; NOISE REDUCTION...
Show More