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Processing and Validating CFD Data for Estimating Inlet Dynamic Total-Pressure Distortion
2020<div class="section abstract"> <div class="htmlview paragraph">The processes addressed in this Aerospace Information Report (AIR) apply to the acquisition and validation of dynamic total-pressure and distortion data from CFD models simulating turbulent flows in inlets.
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Design of a Total Pressure Distortion Generator for Aircraft Engine Testing
2014Master of ...
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Effects of Inlet Total Pressure Distortion on the Performance of a Two-Stage Transonic Fan
Volume 12A: Turbomachinery — Axial Flow Fan and Compressor AerodynamicsAbstract Improving the understanding of the interaction between multistage fan and an inlet total pressure distortion is benefical to design an advanced compression system and stabilizing measures with strong anti-distortion ability. Full-annulus unsteady simulation is applied in a two stage fan to supplement the physic of distorted flow
Jiahui Qiu +5 more
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1976
Abstract : A performance evaluation of an airjet distortion generator system used to produce steady-state, total-pressure distortion at the inlet to a turbine engine was conducted. The capability of the system to duplicate screen- generated, parametric distortion patterns (180 deg, one per revolution; tip radial; hub radial) and to maintain a constant ...
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Abstract : A performance evaluation of an airjet distortion generator system used to produce steady-state, total-pressure distortion at the inlet to a turbine engine was conducted. The capability of the system to duplicate screen- generated, parametric distortion patterns (180 deg, one per revolution; tip radial; hub radial) and to maintain a constant ...
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SAE Technical Paper Series, 2011
<div class="section abstract"><div class="htmlview paragraph">A methodology to evaluate the sensitivity of total pressure intake distortion descriptors defined by SAE ARP 1420 to individual pressure fluctuations in the Aerodynamic Interface Plane -AIP- has been developed.
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<div class="section abstract"><div class="htmlview paragraph">A methodology to evaluate the sensitivity of total pressure intake distortion descriptors defined by SAE ARP 1420 to individual pressure fluctuations in the Aerodynamic Interface Plane -AIP- has been developed.
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2025 5th International Conference on Electrical Engineering and Mechatronics Technology (ICEEMT)
Ye Yang, Xingya Da, Yuan Yi, Junqiang Wu
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Ye Yang, Xingya Da, Yuan Yi, Junqiang Wu
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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2022
Baofeng Tu, Xinyu Zhang
exaly
Baofeng Tu, Xinyu Zhang
exaly

