Numerical investigation on drag and heat reduction mechanism of combined spike and rear opposing jet configuration
Author:
Funder
Priority Academic Program Development of Jiangsu Higher Education Institutions
Publisher
Elsevier BV
Subject
Aerospace Engineering
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1. Numerical investigation of nonlinear aeroelastic characteristics of a supersonic drag-reduction spike;Computers & Fluids;2024-02
2. An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil;International Journal of Turbo & Jet-Engines;2023-04-10
3. Study on hypersonic drag and heat reduction of a spiked blunt body with multiple flat aerodisks and rear opposing jets;Case Studies in Thermal Engineering;2023-02
4. Hybrid technique;Aerodynamic Heating in Supersonic and Hypersonic Flows;2023
5. Coupled Fluid-Thermal Investigation on Drag and Heat Reduction of a Hypersonic Spiked Blunt Body with an Aerodisk;Aerospace;2021-12-30
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