An Improved CFD-synthesis Method for Predicting Inlet Dynamic Distortion-Reference-Cited by-同舟云学术

An Improved CFD-synthesis Method for Predicting Inlet Dynamic Distortion

Published:2009-10 Issue:5 Volume:22 Page:467-473
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Lifen Zhang,Zhenxia Liu,Jiyun Qu,Xiaofeng Wang

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference15 articles.

1. Sedlok D. Improved statistical analysis method for prediction of maximum inlet distortion. AIAA-1984-1274, 1984.

2. Motycka D L. Determination of maximum expected instantaneous distortion patterns from statistical properties of inlet pressure data. AIAA-1976-705, 1976.

3. Forner J A, Manter J M. Prediction of cruise missile inlet peak instantaneous distortion patterns from steady state and turbulence data using a statistical technique. AIAA-1982-1085, 1982.

4. Sanders M E. An evaluation of statistical methods for the prediction of maximum time-variant inlet total pressure distortion. AIAA-1980-1110, 1980.

5. Melick H C Jr, Ybarra A H, Bencze D P. Estimating maximum instantaneous distortion from inlet total pressure RMS and PSD measurements. AIAA-1975-1213, 1975.

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