36th AIAA Aerospace Sciences Meeting and Exhibit 1998
DOI: 10.2514/6.1998-557
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Oscillatory combustion of fine-AP/HTPB propellants

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Cited by 5 publications
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“…Instability research, therefore, requires the use of a nonlinear approach, as the powders themselves are nonlinear systems with certain eigenfrequences and decay rates. Response functions were obtained in experiments by finding the dynamic characteristics of the burning rate; the disturbances were mainly initiated by radiative heat pulses and pressure oscillations in a T-chamber [11][12][13][14][15][16][17][18][19].…”
Section: Introductionmentioning
confidence: 99%
“…Instability research, therefore, requires the use of a nonlinear approach, as the powders themselves are nonlinear systems with certain eigenfrequences and decay rates. Response functions were obtained in experiments by finding the dynamic characteristics of the burning rate; the disturbances were mainly initiated by radiative heat pulses and pressure oscillations in a T-chamber [11][12][13][14][15][16][17][18][19].…”
Section: Introductionmentioning
confidence: 99%