Analysis of jet blast impact of embarked aircraft on deck takeoff zone

K Yue, L Cheng, H Liu, Y Wang - Aerospace Science and Technology, 2015 - Elsevier
The jet blast impact of embarked aircraft on the takeoff zone is studied to support carrier–
aircraft adaptation. The geometric model of carrier–aircraft system is built in CATIA Software …

Numerical investigation of inlet distortion in a jet engine coupled with Ski-jump of carrier-based aircraft

H Wang, Y Lyu, J Zhang, SF Liu - Thermal Science and Engineering …, 2023 - Elsevier
Contract with land-based aviation, the ski-jump of carrier-based aircraft is confronted with
complicated aerodynamic circumstances. More especially, the occurrence of inlet distortion …

Numerical simulation of the aerodynamic influence of an aircraft on the hose-refueling system during aerial refueling operations

K Yue, L Cheng, T Zhang, J Ji, D Yu - Aerospace Science and Technology, 2016 - Elsevier
The aerodynamic characteristics of the flow field of an embarked buddy-refueling aircraft are
analyzed to technically aid the docking between the embarked buddy-refueling aircraft and …

Simulation and experimental analysis of the temperature field of jet flow of aircraft based on CFD theory

Z Chen, W Cai, L Cai, G Cen, H Wang - IEEE Access, 2020 - ieeexplore.ieee.org
As a key indicator of airport concrete pavement, the durability of concrete is seriously
affected by the jet flow generated by aircraft engines. In order to clarify the temperature field …

Prediction of heat affected zone and other mechanical properties of welded joints of HSLA A588-B of jet blast deflector

U Waghmare, AS Dhoble, R Taiwade… - World Journal of …, 2019 - emerald.com
Purpose The purpose of this paper is to predict and optimize the width of heat affected zone
(HAZ) with better mechanical properties using suitable welding process and parameters for …

The effect analysis of an engine jet on an aircraft blast deflector

S Ma, J Tan, X Li, J Hao - … of the Institute of Measurement and …, 2019 - journals.sagepub.com
This paper establishes a novel mathematical model for computing the plume flow field of a
carrier-based aircraft engine. Its objective is to study the impact of jet exhaust gases with …

尾喷流吸入对发动机进气畸变的影响

王俊琦, 汪涛, 刘雨 - 航空动力学报, 2021 - jasp.com.cn
为了研究折返的尾喷流吸入对发动机进口流场畸变的影响特点, 开展了发动机不同状态下的尾喷
流吸入地面试验, 基于测取的发动机进口温度, 压力流场数据, 分析了发动机进口流场温度 …

Numerical Analysis of Air Curtain Jet Blast Deflector

S Fletcher, DK Walters… - ASME …, 2023 - asmedigitalcollection.asme.org
This paper presents the numerical results for a novel proof of-concept jet blast deflector
design based on use of a high-speed air curtain to deflect aircraft engine exhaust gases …

Sinking Velocity Impact‐Analysis for the Carrier‐Based Aircraft Using the Response Surface Method‐Based Improved Kriging Algorithm

XF Xue, YZ Wang, C Lu… - Advances in Materials …, 2020 - Wiley Online Library
The deck landing sinking velocity of carrier‐based aircraft is affected by carrier attitude, sea
condition, aircraft performance, etc. Its impact analysis is a complex nonlinear problem, and …

Numerical investigation on the interaction of a pair of hot off-design supersonic jets with a jet blast deflector

LA Bendersky, DA Lyubimov… - TsAGI Science …, 2018 - dl.begellhouse.com
The interaction of a pair of hot off-design jets from biconical supersonic nozzles is
numerically investigated by the high-resolution RANS/ILES method. The distance between …