Admittance measurements of solid propellants by an acoustic oscillator technique
- 1 June 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (6), 1123-1129
- https://doi.org/10.2514/3.2478
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Use of the one-dimensional t-burner to study oscillatory combustionAIAA Journal, 1964
- T-burner method of determining the acoustic admittance of burning propellantsAIAA Journal, 1964
- PARTICULATE DAMPING OF OSCILLATORY COMBUSTIONAIAA Journal, 1963
- Interaction Between Sound and Flow: Stability of T-BurnersAIAA Journal, 1963
- SCALING PROBLEMS ASSOCIATED WITH UNSTABLE BURNING IN SOLID PROPELLANT ROCKETSPublished by Elsevier ,1963
- VIRTUAL SPECIFIC ACOUSTIC ADMITTANCE MEASUREMENTS OF BURNING SOLID PROPELLANT SURFACES BY A RESONANT TUBE TECHNIQUEPublished by Elsevier ,1963
- DYNAMIC CHARACTERISTICS OF SOLID PROPELLANT COMBUSTIONPublished by Elsevier ,1963
- Solid Propellant Rocket Motors as Acoustic OscillatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1960
- Combustion Instability: Acoustic Interaction with a Burning Propellant SurfaceThe Journal of Chemical Physics, 1959