Zobrazeno 1 - 10 of 18 pro vyhledávání: '"R. L. COATES"'
2
Further Considerations on the Interaction of Sound and Flow in Rocket Motors and T-Burners
Autor: R. L. Coates, M. D. Horton
Publikováno v: Combustion Science and Technology. 9:95-102
An extension of prior theory describing the interaction of steady flow and acoustic oscillations in rocket motors and T-Burners is made. The extension predicts a strong stabilizing effect due to the convection of acoustic energy out of the combustion
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::5728865631730543f033e7b32c83fa41
https://doi.org/10.1080/00102207408960343
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3
An Analysis of a Simplified Laminar Flame Theory for Solid Propellant Combustion
Autor: R. L. Coates
Publikováno v: Combustion Science and Technology. 4:1-8
An approximation to the classical laminar flame theory was proposed by Denison and Baum (1961) which eliminates the need for numerical computation of the burning rate eigenvalue. This approximation is particularly useful in the analysis of non-steady
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::d073e427459b6f7ff5b586bc510272e0
https://doi.org/10.1080/00102207108952466
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5
Thrust magnitude and restart control of solid motors by injection ofhypergolic fluids
Autor: J. H. Bonin, R. L. Coates, N. S. Cohen
Publikováno v: Journal of Spacecraft and Rockets. 4:354-358
A recent experimental program has demonstrated successfully the feasibility of thrust magnitude and stop-restart control of a solid propellant motor using a hypergolic fluid as the control medium. The fluid is injected directly into the combustion ch
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::53bda3eb675dac9aee4612ada8a63184
https://doi.org/10.2514/3.28865
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6
T-burner method of determining the acoustic admittance of burning propellants
Autor: R. L. Coates, N. W. Ryan, M. D. Horton
Publikováno v: AIAA Journal. 2:1119-1122
T-burner experiments have provided the most fruitful technique for obtaining the acoustic admittance of burning solid propellants The objections to the findings of these experiments are: 1) the admittance values are questioned on the grounds that aco
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::91af3266baf42c453e8498f3cdd33e56
https://doi.org/10.2514/3.2477
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7
Acoustic instability - influence of and on the solid phase
Autor: N. W. Ryan, R. L. Coates
Publikováno v: AIAA Journal. 2:1130-1134
In simple terms, acoustic instability in solid propellant rockets is observed as acoustic oscillations in the characteristic modes of the gas cavity driven by the combustion process at the gas-solid interface The effectiveness of the driving process,
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::80c8d07d0ff856c143ba545b6f3ed54b
https://doi.org/10.2514/3.2479
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8
Linear pyrolysis rate measurements of propellant constituents
Autor: R. L. Coates
Publikováno v: AIAA Journal. 3:1257-1261
The effect of chemical erosion on heat-transfer rates can be derived from the net heat of reaction involved and the resulting effect on wall enthalpy. The convective heating rate can be evaluated using the effective wall-enthalpy/ temperature relatio
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ab7b15d9dbae9ef2b11a7a9d8567dfb2
https://doi.org/10.2514/3.3118
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