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Chemically Reacting One-Dimensional Gas-Particle FlowsThe governing equations for the one-dimensional flow of a gas-particle system are discussed. Gas-particle effects are coupled via the system momentum and energy equations with the gas assumed to be chemically frozen or in chemical equilibrium. A computer code for calculating the one-dimensional flow of a gas-particle system is discussed and a user's input guide presented. The computer code provides for the expansion of the gas-particle system from a specified starting velocity and nozzle inlet geometry. Though general in nature, the final output of the code is a startline for initiating the solution of a supersonic gas-particle system in rocket nozzles. The startline includes gasdynamic data defining gaseous startline points from the nozzle centerline to the nozzle wall and particle properties at points along the gaseous startline.
Document ID
19760008175
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tevepaugh, J. A.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Penny, M. M.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
LMSC-HREC-TR-D390876
NASA-CR-147388
Report Number: LMSC-HREC-TR-D390876
Report Number: NASA-CR-147388
Accession Number
76N15263
Funding Number(s)
CONTRACT_GRANT: NAS9-14517
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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