Accession Number:

ADA024984

Title:

Experiments and Analysis Related to External Burning for Propulsion

Descriptive Note:

Interim rept. Feb 1975-Jan 1976

Corporate Author:

GEORGIA INST OF TECH ATLANTA SCHOOL OF AEROSPACE ENGINEERING

Report Date:

1976-03-01

Pagination or Media Count:

62.0

Abstract:

The results of first years efforts on an experimental base flow program are reported. The design and checkout for a Mach 3.0 axisymmetric wind tunnel with a model base diameter of 2.25 inches is described, as well as the automated data acquisition system. Experiments are reported on detailed static pressures for the diffuser wall, model wall and base and near wake. Temperature measurements are presented to establish a near adiabatic wall condition. The relationship between the experimental program and propulsive external burning is discussed.

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Guided Missiles
  • Air Breathing Engines (Unconventional)

Distribution Statement:

APPROVED FOR PUBLIC RELEASE