Accession Number:

AD0291718

Title:

A THIN AIRFOIL WITH A MINIMUM AVERAGE COEFFICIENT OF HEAT TRANSFER FOR A GIVEN LIFT

Descriptive Note:

Technical Report

Corporate Author:

RAND CORP SANTA MONICA CA SANTA MONICA United States

Personal Author(s):

Report Date:

1962-11-01

Pagination or Media Count:

21.0

Abstract:

The transition to high supersonic velocities of flight leads to significant kinetic heating of the wing of an aircraft.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE