An investigation of the flow in turbojet test cells and augmenters
By: by Jack D. Hayes and David W. Netzer
Contributors: Netzer, David Willis, 1939; Naval Postgraduate School (U.S.)
Publisher: Naval Postgraduate School
Published: 1975
Place of publication: Monterey, Calif
Language: eng
Number of pages: 85
Subjects: Airplanes; Testing; Turbojet engines; Air flow
Description: A two-dimensional elliptic computer model was adapted to the solution of the flow field in a turbojet thest 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.
Notes: Title from cover.

"Prepared for: Naval Air Propulsion Test Center"--Cover.

"October 1975"--Cover.

"NPS-57Nt75101"--Cover.

Author(s) subject terms: Turbojet test cell, augmenter, flow model.

Includes bibliographical references (p. 81).

"Approved for public release; distribution unlimited"--Cover.

Technical report; 1975.