Reduction of wave drag on parameterized blunt bodies using spikes with varied tip geometries
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference19 articles.
1. Investigation of the Flow over a Spiked-Nose Hemisphere-Cylinder at a Mach Number of 6.8;Crawford,1959
2. Drag reduction on a spiked body at hypersonic speed;dHumières;Aeronaut. J.,2010
3. Numerical investigation of a spiked blunt nose cone at hypersonic speeds;Gauer;J. Spacecr. Rocket.,2008
4. Navier-Stokes solution for a heat shield with and without a forward facing spike;Mehta;Comput. Fluids,1997
5. Drag reduction for spike attached to blunt-nosed body at mach 6;Kalimuthu;J. Spacecr. Rocket.,2010
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1. Numerical Analysis and Design Optimization Of Bluff Body Using Spike;Journal of Aerospace Sciences and Technologies;2023-07-28
2. Mechanical techniques (spike);Aerodynamic Heating in Supersonic and Hypersonic Flows;2023
3. Hypersonic drag and heat reduction mechanism of a new hybrid method of spike, multi-row discs and opposing jets aerodynamic configuration;International Journal of Heat and Mass Transfer;2022-09
4. Parametric research on drag reduction and thermal protection of blunt-body with opposing jets of forward convergent nozzle in supersonic flows;Acta Astronautica;2022-01
5. An effective means of drag reduction in high enthalpy flow through unsteady energy deposition;Acta Astronautica;2021-09
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