Accession Number:

ADA252711

Title:

Pressure and Temperature for B-1B Transparency Test

Descriptive Note:

Technical memo. Feb 1990-Apr 1991

Corporate Author:

WRIGHT LAB WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1992-05-01

Pagination or Media Count:

122.0

Abstract:

Pressure and temperature data are presented for life cycle testing of the B-lB transparency. For each of three mission types, contour plots of pressure and temperature are presented for each mission segment. Potential flow theory was used to calculate pressure. Isentropic flow was assumed for calculating temperature.

Subject Categories:

  • Aerodynamics
  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE