Accession Number:

AD0762579

Title:

Preliminary Design of a FOA Cryptosteady Energy Separator for Use in Supersonic Aircraft

Descriptive Note:

Corporate Author:

GEORGE WASHINGTON UNIV WASHINGTON DC SCHOOL OF ENGINEERING AND APPLIED SCIENCE

Personal Author(s):

Report Date:

1972-09-01

Pagination or Media Count:

59.0

Abstract:

The report deals with the design of a Foa Energy Separator for use in a supersonic aircraft, the LTV F-8U Crusader. Calculations are carried out to obtain a range of exit nozzle area ratios compatible with a variety of operating conditions. The effects of variations of the peripheral rotor velocity and discharge pressures on both the hot and cold outputs are analyzed. The potential merit of using a heat exchanger in conjunction with the separator, or of using ram air rather than bleed air, is also discussed.

Subject Categories:

  • Attack and Fighter Aircraft
  • Air Conditioning, Heating, Lighting and Ventilating

Distribution Statement:

APPROVED FOR PUBLIC RELEASE