Accession Number : ADA018193

Title :   An Investigation of the Flow in Turbojet Test Cell Augmenters

Descriptive Note : Master's thesis

Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA

Personal Author(s) : Hayes, Jack D

PDF Url : ADA018193

Report Date : Sep 1975

Pagination or Media Count : 83

Abstract : A two-dimensional elliptic computer model was adapted to the solution of the flow field in a turbojet test cell section which contained the engine exhaust duct and augmenter tube. Various engine power settings, augmentation ratios, and augmenter geometries were investigated. Flow visualization and static pressure recovery were primary objectives subject to specified engine power settings and augmentation ratios. Capabilities and limitations of the model are discussed.

Descriptors :   *AIR POLLUTION, *EXHAUST GASES, *JET ENGINES, *TEST FACILITIES, AIR ENTRAINMENT, AUGMENTATION, COMPUTER PROGRAMMING, FLOW FIELDS, THESES

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE