Linear acoustic gains and losses in solid propellant rocket motors-Reference-Cited by-同舟云学术

Linear acoustic gains and losses in solid propellant rocket motors

Published:1964-06 Issue:6 Volume:2 Page:1100-1105
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

CANTRELL R. H.¹,HART R. W.¹,MCCLURE F. T.¹

Affiliation:

1. Applied Physics Laboratory, The Johns Hopkins University, Silver Spring, Md

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.2482

Reference14 articles.

1. Hart, R W and McClure, F T , 'Combustion instability: acoustic interaction with a burning propellant surface, ' J Chem Phys 30, 1501-1514(1959)

2. Bird J F , Haar, L , Hart, R . W , and McClure, F T , "Effect of solid propellant compressibility on combustion instability/ J Chem Phys 32,1423-1429(1960)

3. Hart, R W and Cantrell, R H , "Amplification and at tenuation of sound by burning propellants/ AIAA J 1, 398-404(1963)

4. Cantrell, R H , McClure F T , and Hart, R W , "Acoustic damping in cavities with mean velocity and thermal boundary layers, ' J Acoust Soc Am 35, 500-509 (1963)

5. The effect of compositional variables upon oscillatory combustion of solid rocket propellants

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