Accession Number:

ADA017782

Title:

Thrust Augmenting Ejectors

Descriptive Note:

Technical interim rept. Jan-Jun 1975

Corporate Author:

AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1975-06-01

Pagination or Media Count:

196.0

Abstract:

An overview of ejectors as thrust augmentors is presented including the motivation for and operation of thrust augmenting ejectors. Background studies involving jet mixing and diffusion studies are included as well as the state of the art in unsteady jet interactions. Examples of VSTOL aircraft designs incorporating thrust augmenting ejectors are shown and their advantages discussed.

Subject Categories:

  • VSTOL
  • Fluidics and Fluerics
  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE