Pressure and Temperature for B-1B Transparency Test

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.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1992
Accession Number
ADA252711

Entities

People

  • Elijah W. Turner
  • John T. Riechers

Organizations

  • Wright Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Boundary Layer
  • Computer Programs
  • Computers
  • Cycles
  • Flow
  • Geometry
  • Life Cycle Testing
  • Life Cycles
  • Mach Number
  • Plastic Explosives
  • Potential Flow
  • Structural Integrity
  • Swept Wings
  • Temperature Gradients
  • Three Dimensional
  • Transparencies

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Plasma Physics / Magnetohydrodynamics
  • Structural Health Monitoring of Composite Structures.