INVISCID-INCOMPRESSIBLE-FLOW THEORY OF NORMAL AND SLIGHTLY OBLIQUE IMPINGEMENT OF A STATIC ROUND JET ON THE GROUND,

Abstract

An inviscid-incompressible-flow theory of normal and slightly oblique impingement of a static round jet on the ground is developed and compared with the results of a bench test. The velocity distribution along the ground and across the jet exit, the location of the free stream tube boundary, and thrust ratios at constant power and constant total head are presented as functions of the height of the jet exit above the ground and of the angle of tilt. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1967
Accession Number
AD0648500

Entities

People

  • T. Strand

Tags

DTIC Thesaurus Topics

  • Bench Tests
  • Boundaries
  • Flow
  • Fluid Flow
  • Free Stream
  • Incompressible Flow

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Geodesy