Production SST Parametric Engine Studies - Mission Analysis

Abstract

This document presents the results of a prametric engine cycle study which evaluates the effect of engine cycle on noise and performance of the Production SST. The engine cycles considered are duct burning turbofans, dry turbojets, and afterburning turbojets.

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Document Details

Document Type
Technical Report
Publication Date
Aug 10, 1970
Accession Number
AD0906467

Entities

People

  • A. Moruss

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Afterburning
  • Air Flow
  • Aircrafts
  • Combustion
  • Communities
  • Compressors
  • Engines
  • Governments
  • Jet Aircraft
  • Noise
  • Production
  • Sea Level
  • Supersonic Transport Aircraft
  • Turbofan Engines
  • Turbojet Engines
  • United States

Fields of Study

  • Engineering

Readers

  • Combustion and Flow Dynamics.
  • Software Engineering