Window Systems for Advanced Vehicles

Item

Title
Window Systems for Advanced Vehicles
Date
1964
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
FDL TDR 64-39
Creator
Lis, S. J.
Barile , R. G.
Engholm, G.
Corporate Author
General American Transportation Corporation
Laboratory
Air Force Flight Dynamics Laboratory
Extent
141
Identifier
AD0459373
Access Rights
Notice(s)
Distribution Classification
1
Contract
AF 33(657)-9138
DoD Project
1368
DoD Task
136802
DTIC Record Exists
No
Distribution Change Authority Correspondence
AFFDL LTR
Abstract
A basic investigation to describe the heat transfer and temperature distribution in semi-transparent window materials subjected to simultaneous convective and radiative heat input. The mechanism of heat transfer within the window is treated by separated conductive and radiative modes. Results derived from IBM 7090 Digital Computer Programs are presented for single glaze windows subjected to a hypersonic skip glide trajectory, a supersonic flight and a circular earth orbit. The conditions where radiative interchange is important are studied. Initial results considering the effects of a thin transparent film on a single glazing are presented.
Report Availability
Full text available
Date Issued
1964-12
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource