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Dive into the research topics where Jianwei Mo is active.

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Featured researches published by Jianwei Mo.


Journal of Propulsion and Power | 2014

Design of an Asymmetric Scramjet Nozzle with Circular to Rectangular Shape Transition

Jianwei Mo; Jinglei Xu; Rui Gu; Zhipeng Fan

A novel method for optimizing the shape of a three-dimensional scramjet nozzle with circular to rectangular shape transition, which aims to improve airframe integration, is presented in this paper. To generate the shape of the nozzle, the streamline tracing technique is used based on an annular optimum thrust nozzle flowfield calculated using the method of characteristics. The research is conducted using both the computational fluid dynamics approach and wind-tunnel experiments. Viscous flowfields are computed under the design conditions using commercial software Fluent in order to access the aerodynamic performance of the nozzle. The obtained computational fluid dynamics results on flow static pressures on the upper and lower walls of the three-dimensional nozzle have been validated against the measurement data. Comparisons of the computational fluid dynamics and wind-tunnel experimental results have been conducted under two specific nozzle pressure ratios; that is, underexpansion condition with nozzle p...


Measurement Science and Technology | 2015

New adaptive sampling method in particle image velocimetry

Kaikai Yu; Jinglei Xu; Lan Tang; Jianwei Mo

This study proposes a new adaptive method to enable the number of interrogation windows and their positions in a particle image velocimetry (PIV) image interrogation algorithm to become self-adapted according to the seeding density. The proposed method can relax the constraint of uniform sampling rate and uniform window size commonly adopted in the traditional PIV algorithm. In addition, the positions of the sampling points are redistributed on the basis of the spring force generated by the sampling points. The advantages include control of the number of interrogation windows according to the local seeding density and smoother distribution of sampling points. The reliability of the adaptive sampling method is illustrated by processing synthetic and experimental images. The synthetic example attests to the advantages of the sampling method. Compared with that of the uniform interrogation technique in the experimental application, the spatial resolution is locally enhanced when using the proposed sampling method.


Acta Astronautica | 2015

Design and cold flow test of a scramjet nozzle with nonuniform inflow

Jianwei Mo; Jinglei Xu; Zhibin Quan; Kaikai Yu; Zheng Lv


Archive | 2012

Bypass type double-throat passive vectoring sprayer nozzle

Ming Li; Jinglei Xu; Shunzhou Huang; Rui Gu; Hualin Liao; Yu Fu; Jianwei Mo; Yang Yu


Aerospace Science and Technology | 2015

Inverse design of inlet distortion using method of characteristics for direct-connect scramjet studies

Kaikai Yu; Jinglei Xu; Lan Tang; Jianwei Mo


Acta Astronautica | 2015

Fluid–structure interaction study of the splitter plate in a TBCC exhaust system during mode transition phase

Shuai Guo; Jinglei Xu; Jianwei Mo; Rui Gu; Lina Pang


Aerospace Science and Technology | 2017

A new design method of single expansion ramp nozzles under geometric constraints for scramjets

Zheng Lv; Jinglei Xu; Yang Yu; Jianwei Mo


Shock Waves | 2015

Unsteady transitions of separation patterns in single expansion ramp nozzle

Yang Yu; Jinglei Xu; Kaikai Yu; Jianwei Mo


Acta Astronautica | 2017

Numerical investigation of improving the performance of a single expansion ramp nozzle at off-design conditions by secondary injection

Zheng Lv; Jinglei Xu; Jianwei Mo


Acta Astronautica | 2017

Study of the unsteady mode transition process for an over-under TBCC exhaust system

Zheng Lv; Jinglei Xu; Jianwei Mo

Collaboration


Dive into the Jianwei Mo's collaboration.

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Jinglei Xu

Nanjing University of Aeronautics and Astronautics

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Rui Gu

Nanjing University of Aeronautics and Astronautics

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Zheng Lv

Nanjing University of Aeronautics and Astronautics

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Kaikai Yu

Nanjing University of Aeronautics and Astronautics

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Yang Yu

Nanjing University of Aeronautics and Astronautics

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Lan Tang

Nanjing University of Aeronautics and Astronautics

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Zhibin Quan

Nanjing University of Aeronautics and Astronautics

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Lina Pang

Nanjing University of Aeronautics and Astronautics

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Pu Zhang

Nanjing University of Aeronautics and Astronautics

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Shuai Guo

Nanjing University of Aeronautics and Astronautics

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