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A Control-Volume Method for Analysis of Unsteady Thrust Augmenting Ejector Flows
Contributor(s): Nasa, National Aeronautics and Space Adm (Author)

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 ISBN: 1731496842     ISBN-13: 9781731496843
Publisher: Independently Published
OUR PRICE: $17.09  

Binding Type: Paperback
Published: November 2018
* Out of Print *
Additional Information
BISAC Categories:
- Science | Space Science
Physical Information: 0.36" H x 8.5" W x 11" L (0.90 lbs) 170 pages
 
Descriptions, Reviews, Etc.
Publisher Description:
A method for predicting transient thrust augmenting ejector characteristics is presented. The analysis blends classic self-similar turbulent jet descriptions with a control volume mixing region discretization to solicit transient effects in a new way. Division of the ejector into an inlet, diffuser, and mixing region corresponds with the assumption of viscous-dominated phenomenon in the latter. Inlet and diffuser analyses are simplified by a quasi-steady analysis, justified by the assumptions that pressure is the forcing function in those regions. Details of the theoretical foundation, the solution algorithm, and sample calculations are given. Drummond, Colin K. COMPUTATIONAL FLUID DYNAMICS; COMPUTERIZED SIMULATION; EJECTORS; FINITE VOLUME METHOD; MATHEMATICAL MODELS; THRUST AUGMENTATION; TURBULENT JETS; UNSTEADY FLOW; ALGORITHMS; INLET FLOW; PREDICTION ANALYSIS TECHNIQUES; REAL TIME OPERATION...
 
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