DUCTED PROPELLER ASSAULT TRANSPORT STUDY. DUCT AND PROPELLER ANALYSIS

Abstract

This report contains the results of the ducted propeller studies conducted under Contract No. Nonr 1675' (00). An extensive compressible momentum analysis has been made, for both the static and the in-flight cases, and curves covering the complete results are contained in Appendices A and B.

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Document Details

Document Type
Technical Report
Publication Date
May 15, 1956
Accession Number
AD0102197

Entities

People

  • R. E. Macey

Organizations

  • Bell Aircraft Corporation

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Axial Flow Compressors
  • Contracts
  • Control Systems
  • Engines
  • Geometry
  • Guide Vanes
  • Inlet Guide Vanes
  • Mach Number
  • Propellers
  • Propulsion Systems
  • Shrouded Propellers
  • Static Pressure
  • Turboprop Engines
  • Two Dimensional
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Technical Research and Report Writing.