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Reacting Multi-Species Gas Capability for USM3D Flow Solver
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (08/21/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
The USM3D Navier-Stokes flow solver contributed heavily to the NASA Constellation Project (CxP) as a highly productive computational tool for generating the aerodynamic databases for the Ares I and V launch vehicles and Orion launch abort vehicle (LAV). USM3D is currently limited to ideal-gas flows, which are not adequate for modeling the chemistry or temperature effects of hot-gas jet flows. This task was initiated to create an efficient implementation of multi-species gas and equilibrium chemistry into the USM3D code to improve its predictive capabilities for hot jet impingement effects. The goal of this NASA Engineering and Safety Center (NESC) assessment was to implement and validate a simulation capability to handle real-gas effects in the USM3D code. This document contains the outcome of the NESC assessment. Frink, Neal T. and Schuster, David M. Langley Research Center NASA/TM-2012-217575, NESC-RP-07-037, L-20147, NF1676L-14718 WBS 869021.04.07.01.14
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Product Format
Product Details
ISBN-13:
9798676646394
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
84
Carton Quantity:
48
Product Dimensions:
8.50 x 0.17 x 11.02 inches
Weight:
0.48 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
The USM3D Navier-Stokes flow solver contributed heavily to the NASA Constellation Project (CxP) as a highly productive computational tool for generating the aerodynamic databases for the Ares I and V launch vehicles and Orion launch abort vehicle (LAV). USM3D is currently limited to ideal-gas flows, which are not adequate for modeling the chemistry or temperature effects of hot-gas jet flows. This task was initiated to create an efficient implementation of multi-species gas and equilibrium chemistry into the USM3D code to improve its predictive capabilities for hot jet impingement effects. The goal of this NASA Engineering and Safety Center (NESC) assessment was to implement and validate a simulation capability to handle real-gas effects in the USM3D code. This document contains the outcome of the NESC assessment. Frink, Neal T. and Schuster, David M. Langley Research Center NASA/TM-2012-217575, NESC-RP-07-037, L-20147, NF1676L-14718 WBS 869021.04.07.01.14
Show More