Integrated Compact Engine Flow Path

Abstract

(U) The goal of the Integrated Compact Engine Flow Path program was to fully integrate the aircraft structure and propulsion flowpath. The program evaluated multiple distributed inlets and nozzles to determine if they would allow a better integrated wing and propulsion system, exploiting aerodynamic control possible with engine blowing and suction.

Document Details

Document Type
Accomplishment
Publication Date
Oct 01, 2011
Source ID
b5dab947bcf62d0d5ccfeefa7c6464f4

Tags

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Integrated Circuit Design and Technology.

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