Nonlinear axial combustion instability in solid propellant motors-Reference-Cited by-同舟云学术

Nonlinear axial combustion instability in solid propellant motors

Published:1964-02 Issue:2 Volume:2 Page:275-284
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

BROWNLEE W. G.¹

Affiliation:

1. Canadian Armament Research and Development Establishment, Valcaitier, Quebec, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.2303

Reference11 articles.

1. Jackson, F and Brownlee, W G. "The 9KS11000 rocket engine for the Black Brant III (U), Interim report-First ten firings, Part II-Ballistic design and combustion instability investigations," Canadian Armament Research and Development Establishment Tech Memo 653/62(1962); unclassified

2. Morris, E P , personal communication, Test and Evaluation Section, Propulsion Wing, Canadian Armament Research and Development Establishment (1963)

3. Dickinson, L A , Brownlee, W G , and Jackson, F , "CARDE investigations of finite wave axial combustion instability," Canadian Armament Research and Development Establishment TN 1459/62 (1962); unclassified

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