“…For the subsonic injection, we omitted the data for the downstream half of the laser cavity due to large measurement error. As predicted by thermal analysis, 7) the gas medium for subsonic injection has a higher heat release and a higher temperature than that for transonic injection. In both schemes, increasing the iodine flow rate results in an increase in temperature.…”
Section: Temperature In the Laser Cavity And Heat Releasementioning
confidence: 77%
“…( 3) represent the heat per unit of time released from the gas mixture, and the terms on the right-hand are defined as follows: q Á n I 2 FN is the energy released from O 2 ( 1 Á) during the iodine dissociation, q I 2 n I 2 F is the energy consumed by molecular iodine for the dissociation, and q I Ã n I 2 F Á 2K e Y= fðK e À 1ÞY þ 1g is the energy consumed by atomic iodine for the excitation. The stagnation temperature of the primary flow T 0ip was determined by gasdynamic method 7) from the experiments without secondary flow and was found to be approximately 300 K. For the secondary flow, T 0is was close to the temperature of the iodine supplying duct, because the gas traveled inside the duct at low subsonic speed. The pipes were preheated up to 100 C in order to avoid iodine condensation, so T 0is was taken as 373 K. The last unknown parameter is the stagnation temperature in the laser cavity T 0 .…”
Section: Analytical Model For the Estimation Of F And Nmentioning
confidence: 99%
“…The cavity temperature calculated while the pressure broadening taking into account is in agreement with the data obtained by the gasdynamic model. 7)…”
Section: Calculation Of Temperaturementioning
confidence: 99%
“…Experimental measurement of temperature made it possible to check the accuracy of the heat release evaluation performed. 7) The results of temperature measurement for subsonic and transonic injections are shown in Figs. 4 and 5, respectively.…”
Section: Temperature In the Laser Cavity And Heat Releasementioning
confidence: 99%
“…As the static pressure inside the cavity changes along the flow, we can estimate T 0 only at the point 7 cm downstream from the NEP, where the pressure gage is installed. This estimation was performed using the model described in our paper, 7) and the values of T 0 are listed in the Table III, which lists the results for eqs. ( 1)-( 3).…”
Section: Analytical Model For the Estimation Of F And Nmentioning
The present study compares the laser medium properties for subsonic and transonic iodine injection schemes of a multi-kW grid-nozzle supersonic chemical oxygen iodine laser (COIL). Two supersonic nozzles of similar geometry having subsonic or transonic iodine injectors were investigated in the present study. Small signal gain (SSG) and internal cavity temperature (ICT) were experimentally measured as a function of the iodine flow rate and coordinate in the direction of the gas flow. Dissociated fraction of iodine F and the number N of O2(1Δ) molecules consumed for the dissociation of one iodine molecule were estimated by an analytical method, utilizing SSG and ICT as input parameters. Both gain and temperature were measured by diode laser spectroscopy. Pressure broadening of the spectroscopic line of iodine atom was taken into account when calculating the gas temperature in the cavity.
“…For the subsonic injection, we omitted the data for the downstream half of the laser cavity due to large measurement error. As predicted by thermal analysis, 7) the gas medium for subsonic injection has a higher heat release and a higher temperature than that for transonic injection. In both schemes, increasing the iodine flow rate results in an increase in temperature.…”
Section: Temperature In the Laser Cavity And Heat Releasementioning
confidence: 77%
“…( 3) represent the heat per unit of time released from the gas mixture, and the terms on the right-hand are defined as follows: q Á n I 2 FN is the energy released from O 2 ( 1 Á) during the iodine dissociation, q I 2 n I 2 F is the energy consumed by molecular iodine for the dissociation, and q I Ã n I 2 F Á 2K e Y= fðK e À 1ÞY þ 1g is the energy consumed by atomic iodine for the excitation. The stagnation temperature of the primary flow T 0ip was determined by gasdynamic method 7) from the experiments without secondary flow and was found to be approximately 300 K. For the secondary flow, T 0is was close to the temperature of the iodine supplying duct, because the gas traveled inside the duct at low subsonic speed. The pipes were preheated up to 100 C in order to avoid iodine condensation, so T 0is was taken as 373 K. The last unknown parameter is the stagnation temperature in the laser cavity T 0 .…”
Section: Analytical Model For the Estimation Of F And Nmentioning
confidence: 99%
“…The cavity temperature calculated while the pressure broadening taking into account is in agreement with the data obtained by the gasdynamic model. 7)…”
Section: Calculation Of Temperaturementioning
confidence: 99%
“…Experimental measurement of temperature made it possible to check the accuracy of the heat release evaluation performed. 7) The results of temperature measurement for subsonic and transonic injections are shown in Figs. 4 and 5, respectively.…”
Section: Temperature In the Laser Cavity And Heat Releasementioning
confidence: 99%
“…As the static pressure inside the cavity changes along the flow, we can estimate T 0 only at the point 7 cm downstream from the NEP, where the pressure gage is installed. This estimation was performed using the model described in our paper, 7) and the values of T 0 are listed in the Table III, which lists the results for eqs. ( 1)-( 3).…”
Section: Analytical Model For the Estimation Of F And Nmentioning
The present study compares the laser medium properties for subsonic and transonic iodine injection schemes of a multi-kW grid-nozzle supersonic chemical oxygen iodine laser (COIL). Two supersonic nozzles of similar geometry having subsonic or transonic iodine injectors were investigated in the present study. Small signal gain (SSG) and internal cavity temperature (ICT) were experimentally measured as a function of the iodine flow rate and coordinate in the direction of the gas flow. Dissociated fraction of iodine F and the number N of O2(1Δ) molecules consumed for the dissociation of one iodine molecule were estimated by an analytical method, utilizing SSG and ICT as input parameters. Both gain and temperature were measured by diode laser spectroscopy. Pressure broadening of the spectroscopic line of iodine atom was taken into account when calculating the gas temperature in the cavity.
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