ANNULAR NOZZLE EJECTOR

Abstract

A study was made of the annular ejector to determine a configuration that accomplishes the following: equals or improves out of ground effect performance; gives superior performance in ground effect; and overcomes the performance loss during ground effect transition. An investigation was made of the combined possibilities of a conically divergent annular primary jet, wide angle augmenter tube, and flow control vanes. The particular primary nozzle geometry chosen (jet aspect ratio, jet divergence angle and area ratio) did not combine effectively with wide angle augmenters to achieve an ejector with out of ground effect performance superior. The investigation also include d the use of vanes at the bellmouth and augmenter inlets and a the aug enter exit. Proper use of the vanes reduced the augmentation loss in ground effect transition to approximately 1/3 the loss without vanes. Full-scale ejector tests indicated that bellmouth losses chargeable to lip separation could be eliminated by a flat lip extension.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1961
Accession Number
AD0278535

Entities

People

  • J. W. Fairbanks
  • M. F. Gates

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Annular Nozzles
  • Aspect Ratio
  • Boundary Layer
  • Contracts
  • Diffusion
  • Flow Rate
  • Flow Visualization
  • Geometry
  • Ground Effect
  • Hypervelocity Flow
  • Measurement
  • Pressure Distribution
  • Secondary Flow
  • Static Pressure
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Engineering
  • Physics

Readers

  • Combustion and Flow Dynamics.