Design considerations for combustion stability.
- 1 March 1969
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 6 (3) , 296-302
- https://doi.org/10.2514/3.29588
Abstract
No abstract availableKeywords
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- Application of the T-burner to ballistic evaluation of new propellants.Journal of Spacecraft and Rockets, 1966
- T-burner method of determining the acoustic admittance of burning propellantsAIAA Journal, 1964
- Nonlinear axial combustion instability in solid propellant motorsAIAA Journal, 1964
- Axial mode, intermediate frequency combustion instability in solid propellant rocket motorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964
- The Absorption of Sound in Suspensions and Emulsions. I. Water Fog in AirThe Journal of the Acoustical Society of America, 1953