1 |
Boyle, D.K., Henderson, B.S. and Hultgren, L.S., "Core/Combustor-Noise Baseline Measurements for the DGEN Aeropropulsion Research Turbofan," Presented at the 2018 AIAA/CEAS Aeroacoustics Conference, Atlanta, Georgia, 2018.
|
2 |
Beltman, W.M., "Viscothermal Wave Propagation Including Acousto elastic Interaction," PhD thesis. University of Twente, 1998.
|
3 |
Gordon, S. and McBride, B.J., Computer Program for Calculation Complex Chemical Equilibrium Compositions and Applications, Publication NASA RP 1311. 1994, p. 64.
|
4 |
Rocket Motor ICP® Pressure Sensor, Installation and Operating Manual. PCB Piezotronics, Inc.
|
5 |
Armbruster, W., Hardi, J., Suslov, D. and Oschwald, M., "High-Speed Flame Radiation Imaging of Thermoacoustic Coupling in a High Pressure Research Thrust Chamber," Presented at the 2018 Joint Propulsion Conference, Cincinnati, Ohio, 2018.
|
6 |
Van de Wyer, N., Brouckaert, J.F. and Miorini, R.L., "On the Determination of the Transfer Function of Infinite Line Pressure Probes for Turbomachinery Applications," Presented at the ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, Copenhagen, Denmark, 2012.
|
7 |
Samuelson, R.D., Pneumatic Instrumentation Lines and Their Use in Measuring Rocket Nozzle Pressure, Publication RN-DR-0124, 4212042. Nuclear Rocket Operations, Aerojet-General Corporation, 1967, p. RN-DR--0124, 4212042.
|
8 |
Taback, I., The Response of Pressure Measuring Systems to Oscillating Pressures, Publication Technical Note NO. 1819. Langley Aeronautical Laboratory Langley Air Force Base, Va., 1949.
|
9 |
Iberall, A.S., "Attenuation of Oscillatory Pressures in Instrument Lines," Journal of Research of the National Bureau of Standards, Vol. 45, No. 1, p. 85, 1950, doi:10.6028/jres.045.008.
DOI
|
10 |
Bergh, H. and Tijdeman, H., "Theoretical and Experimental Results for the Dynamic Response of Pressure Measuring Systems," Publication Report. NLR-TR-F. 238. National Aero and Astronautical Research Institute(NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM), 1965.
|
11 |
Zinn, H. and Habermann, M., "Developments and Experiences With Pulsation Measurements for Heavy-Duty Gas Turbines," Presented at the ASME Turbo Expo 2007: Power for Land, Sea, and Air, Montreal, Canada, 2007.
|
12 |
High Temperature Pressure Sensor for Gas Turbine- and Thermoacoustics Applications. Kistler.
|
13 |
Naples, A., Knisely, A. M., Hoke, J. and Schauer, F., "Infinite Line Pressure Probe and Flush Transducer Measurements in a Rotating Detonation Engine Channel," Presented at the AIAA Scitech 2019 Forum, San Diego, California, 2019.
|
14 |
Salikuddin, M., Burrin, R. and Brown, W., "Design and Characterization of a High Temperature and High Frequency Infinite-Line Pressure Probe," Presented at the 12th Aeroacoustic Conference, San Antonio, TX, U.S.A., 1989.
|
15 |
Kim, H. and Choi, H.S., "A Comparative Study of Frequency Response Models for Pressure Transmission System," Journal of the Korean Society of Propulsion Engineers, Vol. 24, No. 2, 2020, pp. 83-93. doi:10.6108/KSPE.2020.24.2.083.
DOI
|
16 |
Armbruster, W., Groning, S., Hardi, J. and Oschwald, M., "Analysis of High Amplitude Acoustic Pressure FIeld Dynamics in a LOX/H2 Rocket Combustor," p. 12.
|
17 |
Boyle, D.K., Henderson, B.S. and Hultgren, L.S., "Transfer-Function Determination for Infinite-Tube-Probe Pressure Transducers with Application to Turbofan Core/Combustor Noise," Presented at the 25th AIAA/CEAS Aeroacoustics Conference, Delft, The Netherlands, 2019.
|
18 |
Wegner, M., Nance, D. and Ahuja, K., "Characterization of Short and Infinite-Line Pressure Probes for In-Duct Acoustic Measurements Under Hostile Environment," Presented at the 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), Rome, Italy, 2007.
|
19 |
Englund, R. and Richards, W.B., The Infinite Line Pressure Probe, Publication NASA Technical Memorandum 83582. 1984, p. 17.
|
20 |
Naples, A., Hoke, J.L. and Schauer, F.R., "Quantification of Infinite Line Pressure Probe Response to Shocks and Detonation Waves," Presented at the 2018 AIAA Aerospace Sciences Meeting, Kissimmee, Florida, 2018.
|
21 |
Spurling, J.A., "Using a Semi-Infinite Tube to Measure Pressure Oscillations in Solid Rocket Motors," Presented at the 51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, 2015.
|
22 |
Gejji, R.M., Walters, I.V., Beard, S., Lemcherfi, A., Sardeshmukh, S.V., Heister, S.D. and Slabaugh, C.D., "Transducer Installation Effects on Pressure Measurements in PGC Devices," Presented at the 2018 AIAA Aerospace Sciences Meeting, Kissimmee, Florida, 2018.
|
23 |
Ferrara, G., Ferrari, L. and Sonni, G., "Experimental Characterization of a Remoting System for Dynamic Pressure Sensors," Presented at the ASME Turbo Expo 2005: Power for Land, Sea, and Air, Reno, Nevada, USA, 2005.
|
24 |
Blackshear, P.L., Rayle, W.D. and Tower, L.K., Study of Screeching Combustion in a 6-Inch Simulated Afterburner, Publication NACA TN 3567. 1955, p. 60.
|
25 |
Salikuddin, M., "Application of Impedance Tube Technique in the Measurement of Burning Solid Propellant Admittances," Ph.D. Thesis. Georgia Institute of Technology, 1978.
|