AN APPROXIMATE INVESTIGATION OF THE EFFECT OF BOUNDARY LAYER CONTROL PUMPING ON POWERPLANT PERFORMANCE,

Abstract

A first-order analysis is described of the effects of boundary layer bleed pumping on the performance of turbojet and turboprop powerplants.

Document Details

Document Type
Technical Report
Publication Date
Apr 25, 1960
Accession Number
AD0616658

Entities

People

  • T. F. Kirkwood

Organizations

  • RAND Corporation

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Boundary Layer Control
  • Energy Generators
  • Energy Systems
  • Engines
  • Gas Turbines
  • Generators
  • Heat Engines
  • Heat Transfer Devices
  • Internal Combustion Engines
  • Jet Aircraft
  • Jet Engines
  • Layers
  • Turbojet Engines
  • Turboprop Engines

Fields of Study

  • Physics