File:A computer code (SKINTEMP) for predicting transient missile and aircraft heat transfer characteristics (IA acomputercodeski1094530889).pdf
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Summary[edit]
A computer code (SKINTEMP) for predicting transient missile and aircraft heat transfer characteristics ( ) | |
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Author |
Cummings, Mary L. |
Title |
A computer code (SKINTEMP) for predicting transient missile and aircraft heat transfer characteristics |
Publisher |
Monterey, California. Naval Postgraduate School |
Description |
A FORTRAN computer code (SKINTEMP) has been developed to calculate transient missile/aircraft aerodynamic heating parameters utilizing basic flight parameters such as altitude, Mach number, and angle of attack. The insulated skin temperature of a vehicle surface on either the fuselage (axisymmetric body) or wing (two-dimensional body) is computed from a basic heat balance relationship throughout the entire spectrum (subsonic, transonic, supersonic, hypersonic) of flight. This calculation method employs a simple finite difference procedure which considers radiation, forced convection, and non-reactive chemistry. Surfact. pressure estimates are based on a modified Newtonian flow model. Eckert's reference temperature method is used as the forced convection heat transfer model. SKINTEMP predictions are compared with a limited number of test cases. SKINTEMP was developed as a tool to enhance the conceptual design process of high speed missiles and aircraft. Recommendations are made for possible future development of SKINTEMP to further support the design process. Subjects: Mission Critical Computer Resources (MCCR), Software Development, Enhanced Position Location Reporting System (EPLRS), Software Engineering Institute (SEI), Army Data Distribution System (ADDS), Technical Test, Prototpe Qualification Test-Contractor (PQT-C) |
Language | English |
Publication date |
September 1994 publication_date QS:P577,+1994-09-00T00:00:00Z/10 |
Current location |
IA Collections: navalpostgraduateschoollibrary; fedlink |
Accession number |
acomputercodeski1094530889 |
Source | |
Permission (Reusing this file) |
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted. |
Licensing[edit]
Public domainPublic domainfalsefalse |
This work is in the public domain in the United States because it is a work prepared by an officer or employee of the United States Government as part of that person’s official duties under the terms of Title 17, Chapter 1, Section 105 of the US Code.
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This file has been identified as being free of known restrictions under copyright law, including all related and neighboring rights. |
https://creativecommons.org/publicdomain/mark/1.0/PDMCreative Commons Public Domain Mark 1.0falsefalse
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Short title | A computer code (SKINTEMP) for predicting transient missile and aircraft heat transfer characteristics |
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Author | Cummings, Mary L. |
Software used | Cummings, Mary L. |
Conversion program | Mac OS X 10.10.5 Quartz PDFContext |
Encrypted | no |
Page size | 612 x 792 pts (letter) |
Version of PDF format | 1.4 |