Combustion instability in turbojet and turbofan augmentors-Reference-Cited by-同舟云学术

Combustion instability in turbojet and turbofan augmentors

Published:1971-06-14 Issue: Volume: Page:
ISSN:
Container-title:7th Propulsion Joint Specialist Conference
language:
Short-container-title:

Author:

BONNELL J.¹,MARSHALL R.¹,RIECKE G.¹

Affiliation:

1. UNITED AIRCRAFT CORP.,PRATT AND WHITNEY AIRCRAFT DIV., EAST HARTFORD, CONN.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1971-698

Reference9 articles.

1. Lewis Laboratory Staff, "Summaryof Preliminary Investigations into the Characteristics of Combustion Screech in Ducted Burners," NACA Report 1384, 1954.

2. Evaluation of absorption liners for suppression of combustion instability in rocket engines.

3. Clapp, C, J. "Full Scale Turbofan Duct Burner Test Program,11PWAFR-2542, NASACR-54637, 1967.

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