AN EXPERIMENTAL INVESTIGATION OF THE USE OF HOT GAS EJECTORS FOR BOUNDARY LAYER CONTROL

Abstract

The primary purpose of Phase II of the ejector study has been to provide experimental data for engineering design purposes. The geometric and state parameters of the ejector were investigated over a wide range, both with and wfthaut diffuser. Variation in the ejector performance was determined for a change in primary temperature, and the effect of the use of a supersonic primary nozzle was also investigated. Comparisons of theoretical and experimental pumping performance without diffuser are presented.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1953
Accession Number
AD0054379

Entities

People

  • Richard D. Wood
  • Richard V. Deleo

Organizations

  • University of Minnesota

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Barometric Pressure
  • Boundary Layer
  • Boundary Layer Control
  • Combustion
  • Engineering
  • Exhaust Nozzles
  • Experimental Data
  • Heat Transfer
  • Jet Aircraft
  • Jet Engines
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Static Pressure

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow