Unique Operating Conditions Analysis of Turboshaft Engines Based on Nonlinear Integrated Model

References

• B. Sunden and G. Xie, “Gas turbine blade tip heat transfer and cooling: a literature survey,” Heat Transfer Eng., vol. 31, no. 7, pp. 527–554, Jun. 2010. DOI: 10.1080/01457630903425320.
   Web of Science ®Google Scholar
• H. J. Nam, Y. M. Park and O. J. Kwon, “Simulation of unsteady rotor–fuselage aerodynamic interaction using unstructured adaptive meshes,” J. Am. Helicopter Soc., vol. 51, no. 2, pp. 141–149, Apr. 2006. DOI: 10.4050/JAHS.51.141.
   Web of Science ®Google Scholar
• F. Lou, J. C. Fabian and N. L. Key, “Experimental investigation of flow distortion in an auxiliary-power-unit-style inlet system,” J. Propulsion Power, vol. 32, no. 4, pp. 892–902, Jul. 2016. DOI: 10.2514/1.B35948.
   Web of Science ®Google Scholar
• G. Srinivasa Rao and A. Shaija, “Computational analysis of reacting flows in afterburner,” Heat Transfer Engineering, vol. 41, no. 6–7, pp. 576–594, Apr. 2020. DOI: 10.1080/01457632.2018.1546946.
   Web of Science ®Google Scholar
• A. Hashemi and E. Dyson, “Performance characterization of high-power electronic equipment onboard an aircraft,” Heat Transfer Engineering, vol. 21, no. 1, pp. 15–24, Jan. 2000. DOI: 10.1080/014576300271121.
   Web of Science ®Google Scholar
• J. P. Murphy, D. G. MacManus and C. T. Sheaf, “Experimental investigation of intake ground vortices during takeoff,” Aiaa J., vol. 48, no. 3, pp. 688–701, Mar. 2010. DOI: 10.2514/1.45896.
   Google Scholar
• H.-X. Huang, et al., “Flowfield of a helicopter submerged inlet with power output shaft,” Acta Mech. Sin, vol. 37, no. 1, pp. 156–168, Jan. 2021. DOI: 10.1007/s10409-020-01029-z.
   Web of Science ®Google Scholar
• L. Zivan and M. B. Tischler, “Development of a full flight envelope helicopter simulation using system identification,” J Am Helicopter Soc, vol. 55, no. 2, pp. 22003–2200315, Apr. 2010. DOI: 10.4050/JAHS.55.022003.
   Web of Science ®Google Scholar
• A. J. Landgrebe, R. B. Taylor, T. A. Egolf and J. C. Bennett, “Helicopter airflow and wake characteristics for low speed and hovering flight,” J Am Helicopter Soc, vol. 27, no. 4, pp. 74–83, Oct. 1982. DOI: 10.4050/JAHS.27.74.
   Google Scholar
• V. K. Lakshminarayan, T. S. Kalra and J. D. Baeder, “Detailed computational investigation of a hovering microscale rotor in ground effect,” Aiaa J., vol. 51, no. 4, pp. 893–909, Apr. 2013. DOI: 10.2514/1.J051789.
   Google Scholar
• M. Bolemant and D. Peitsch, An Alternative Compressor Modeling Method within Gas Turbine Performance Simulations, 2014, Deutscher Luft-und Raumfahrtkongress 2014, Document ID: 340047 (pp. 12). https://www.dglr.de/publikationen/2014/340047.pdf.
   Google Scholar
• J. K. Lytle, The Numerical Propulsion System Simulation: A Multidisciplinary Design System for Aerospace Vehicles, 1999, NASA Glenn Research Center, Cleveland, Ohio. NASA/TM–1999-209194.
   Google Scholar
• J. K. Lytle, The Numerical Propulsion Simulation: An Overview, 2000, NASA Glenn Research Center, Cleveland, Ohio. NASA/TM–2000-209915.
   Google Scholar
• A. Evans, G. Follen, C. Naiman and I. Lopez, “Numerical propulsion system simulation’s national cycle program,” 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998. In Cleveland, OH, U.S.A.: American Institute of Aeronautics and Astronautics, Jul. paper no. AIAA-98-3113, DOI: 10.2514/6.1998-3113.
   Google Scholar
• J. P. Veres, Overview of High-Fidelity Modeling Activities in the Numerical Propulsion System Simulations (NPSS) Project, 2002, Glenn Research Center, Cleveland, Ohio, NASA/TM—2002-211351.
   Google Scholar
• H. Pearson and A. B. McKenzie, “Wakes in axial compressors,” Aeronautical J., vol. 63, no. 583, pp. 415–416, Jul. 1959. DOI: 10.1017/S0368393100071273.
   Google Scholar
• C. Reid, “The response of axial flow compressors to intake flow distortion,” ASME 1969 Gas Turbine Conference and Products Show, 1969. in Cleveland, Ohio, USA: American Society of Mechanical Engineers, Mar. paper no. 69-GT-29, V001T01A029. DOI: 10.1115/69-GT-29.
   Google Scholar
• J. A. Korn, “Compressor distortion estimates using parallel compressor theory and stall delay,” J. Aircraft, vol. 11, no. 9, pp. 584–586, Sep. 1974. DOI: 10.2514/3.60390.
   Google Scholar
• R. S. Mazzawy, “Multiple segment parallel compressor model for circumferential flow distortion,” J. Eng. Power, vol. 99, no. 2, pp. 288–296, Apr. 1977. DOI: 10.1115/1.3446288.
   Google Scholar
• H. C. Melick, Analysis of Inlet Flow Distortion and Turbulence Effects on Compressor Stability, National Aeronautics and Space Administration Ames Research Centre, Moffett Field, California, 1973, NASA-CR-114577.
   Google Scholar
• H. C. Curtiss, M. Sun, W. F. Putman and E. J. Hanker, “Rotor aerodynamics in ground effect at low advance ratios,” J. Am. Helicopter Soc., vol. 29, no. 1, pp. 48–55, Jan. 1984. DOI: 10.4050/JAHS.29.48.
   Google Scholar
• F. Holzäpfel and M. Steen, “Aircraft wake-vortex evolution in ground proximity: analysis and parameterization,” Aiaa J., vol. 45, no. 1, pp. 218–227, Jan. 2007. DOI: 10.2514/1.23917.
   Google Scholar