NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Comparison of quick-look plume heating calculations and Monte Carlo direct simulationA quick-look method has been developed for estimating convective heat flux due to plume impingement in the transition flow regime on a concave surface surrounding a rocket nozzle. Comparison with the flowfield and heat fluxes computed by the Monte Carlo Direct Simulation Method show the quick-look method to be conservative. Assumptions regarding the nature of the flowfield based on engineering judgment were shown to be essentially valid. Further, the assumption of free molecular impingement was shown to be non-conservative for portions of the surface. Potential refinements of the quick-look method are discussed.
Document ID
19800057308
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Guernsey, C. S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hrubes, J. D.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 10, 2013
Publication Date
July 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 80-1516
Meeting Information
Meeting: Thermophysics Conference
Location: Snowmass, CO
Start Date: July 14, 1980
End Date: July 16, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A41478
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available