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