Gas Turbine Compressor Development Program for 1.5/3 KW Generator Set.

Abstract

This report summarizes a study that performed the preliminary design of a small gas turbine engine, capable of providing 6-hp for driving a 1.5/3 Kw generator set, and presents the results of performance testing the resultant compressor design. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1975
Accession Number
ADA033577

Entities

People

  • Eugene A. Zanelli
  • Jessie B. Lee

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Assembly
  • Boundary Layer
  • Calorific Value
  • Computer Programs
  • Engine Components
  • Engineering
  • Fabrication
  • Gas Turbines
  • Journal Bearings
  • Manufacturing
  • Materials
  • Measurement
  • Performance Tests
  • Plastic Explosives
  • Three Dimensional
  • Turbine Components
  • Turbines

Readers

  • Electrical Engineering