Evaluation of Ultrasound Technique for Solid-Propellant Burning-Rate Response Measurements-Reference-Cited by-同舟云学术

Evaluation of Ultrasound Technique for Solid-Propellant Burning-Rate Response Measurements

Published:2002-05 Issue:3 Volume:18 Page:641-651
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Murphy Jeffrey J.¹,Krier Herman¹

Affiliation:

1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.5978

Reference66 articles.

1. Ho, P. J. “Feasibility Study of the Microwave and the Ultrasonic Techniques on the Continuous Measurement of Solid Propellant Burning Rates,” M.S. Thesis,Purdue Univ., West Lafayette, IN, Aug. 1965.

2. Hale, H. J. “The Demonstration of an Ultrasonic Technique to Measure Solid Propellant Burning Rates Under Actual Combustion Conditions,”M.S. Thesis, Virginia Polytechnic Inst.and State Univ., Blacksburg, VA,June 1967.

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