Investigation on Jet Characteristics of Turbofan Exhaust System under Take-off Condition with High Angle of Attack
To understand the jet flow characteristics of turbofan separate exhaust system, a parametric design method based on the initial Class Shape Transformation function was developed. HBPR and UHBPR turbofan separate exhaust systems were designed. Furthermore, the jet flow characteristics of the HBPR tur...
Main Authors: | Z. X. Wang, W. J. Wang, L. Zhou, W. J. Deng, J. W. Shi |
---|---|
Format: | Article |
Language: | English |
Published: |
Isfahan University of Technology
2022-03-01
|
Series: | Journal of Applied Fluid Mechanics |
Subjects: | |
Online Access: | https://www.jafmonline.net/article_2041_9dcf149579813b7376f3fcf42da4ba6c.pdf |
Similar Items
-
Technologies for jet noise reduction in turbofan engines
by: Mofid Gorji-Bandpy, et al.
Published: (2012-04-01) -
Active Jet Noise Control of Turbofan Engine Based on Explicit Model Predictive Control
by: Runmin Ji, et al.
Published: (2022-05-01) -
Investigation on Infrared Radiation Signatures of Under-Expanded Rocket Exhaust Plumes Due to Angle of Attack
by: Qinglin Niu, et al.
Published: (2021-01-01) -
Study on Overall Parameter and Performance Analysis of Different Configurations for Civil Turbofan Engine
by: Xue Bingjing, et al.
Published: (2018-08-01) -
Parametric Study of a Turbofan Engine with an Auxiliary High-Pressure Bypass
by: Sharanabasaweshwara A. Asundi, et al.
Published: (2019-01-01)