Verification of Nozzle Admittance Theory by Direct Measurement of the Admittance Parameter
- 1 June 1961
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in ARS Journal
- Vol. 31 (6), 771-775
- https://doi.org/10.2514/8.5627
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Theory of Liquid PropelIant Rocket Combustion Instability and Its Experimental VerificationARS Journal, 1960
- TRANSVERSE WAVE AND ENTROPY WAVE COMBUSTION INSTABILITY IN LIQUID PROPELLANT ROCKETSPublished by Defense Technical Information Center (DTIC) ,1957