Thrust Vector Control, Heat Transfer Modeling
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Authors
Leitner, Amiram
Subjects
THRUST VECTOR CONTROL SYSTEMS
MODELS
HEAT TRANSFER
CODING
COEFFICIENTS
SUPERSONIC FLOW
BLUNT BODIES
COMPUTER PROGRAMMING
TWO DIMENSIONAL
NUMERICAL ANALYSI|Thermodynamics
Rocket Engines
MODELS
HEAT TRANSFER
CODING
COEFFICIENTS
SUPERSONIC FLOW
BLUNT BODIES
COMPUTER PROGRAMMING
TWO DIMENSIONAL
NUMERICAL ANALYSI|Thermodynamics
Rocket Engines
Advisors
Date of Issue
1986-07
Date
1986-07
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
The report presents heat transfer modeling of Thrust Vector control systems using the PHOENICS computer code. Simple two-dimensional wedged blunt bodies have been examined in supersonic cold flow, for both laminar and turbulent flow cases. The research presents a numerical solution of the supersonic compressible viscous two-dimensional flow field. Post calculations were done to estimate skin friction coefficient, surface heat flux, heat transfer coefficient and Stanton number distributions in both wedge and blunt cases.
Type
Technical Report
Description
Contractor Report
Series/Report No
Department
Mechanical Engineering (ME)
Organization
Identifiers
NPS Report Number
NPS69-86-005
Sponsors
The work presented in this report is part of a project sponsored by Naval Weapons Center on heat transfer modelin
Funder
Contract Number N62271-86-M-0206
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.