INVESTIGATION OF NEW M.E.I. NOZZLE CASCADES FOR SUPERSONIC VELOCITIES

Abstract

Recommendations are made for the design of nozzle cascades which are distinguished by high efficiency over a wide range of supersonic velocities. Results of investigations of new cascades are given for Mach numbers from 0.6 to 1.8.

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Document Details

Document Type
Technical Report
Publication Date
Mar 04, 1963
Accession Number
AD0400549

Entities

People

  • A. Dzhaganmakhan
  • A. V. Gubarev
  • L. Ya. Lazarev
  • M. Ye. Deych

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Boundary Layer
  • Curvature
  • Efficiency
  • Equations
  • Experimental Data
  • Flow
  • Foreign Technology
  • Gas Flow
  • Government Procurement
  • Governments
  • Mach Number
  • Personality
  • Shape
  • Transverse

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Defense Acquisition Program Management

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow