A Thermal Analysis of an F/A-18 Wing Section for Actuator Thermal Management Thermacore, Incorporated

Format:

Conference/Event

Author/Creator:

Gernert, Nelson J., author.

Conference Name:

Aerospace Atlantic Conference & Exposition (1992-04-01 : Dayton, Ohio, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1992

Summary:

This paper presents the design and performance of a flexible heat pipe cold plate (FHPCP) that was developed for transporting heat from electronics mounted directly on an F/A-18 aileron actuator to a nearby heat sink. The most obvious heat sink is surrounding structure. A one dimensional steady state heat conduction analysis presented in this paper indicates that utilizing structure is feasible for this application

Notes:

Vendor supplied data

Publisher Number:

921023

Access Restriction:

Restricted for use by site license