Temperature Issues for a Mach 2.4 High Speed Civil Transport Boeing Commercial Airplane Group

Format:

Conference/Event

Author/Creator:

Johnson, Bryan D., author.

Conference Name:

Aerospace Technology Conference & Exposition (1994-10-01 : San Diego, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1994

Summary:

The High Speed Civil Transport (HSCT) will be exposed to elevated temperatures during Mach 2.4 supersonic flight. While not as extreme as those encountered in other high speed flight efforts (NASP, Shuttle), thermal effects will impact decisions in almost all areas of material selection and design. Accurate temperatures are required to evaluate materials, structural concepts, cooling requirements, et cetera Analyses show the importance of structural configuration, use of fuel as a heat sink, and surface properties on structural temperatures. Capability to accurately determine convection and radiation boundary conditions is important for future HSCT design

Notes:

Vendor supplied data

Publisher Number:

942160

Access Restriction:

Restricted for use by site license