Navier-Stokes solution for a heat shield with and without a forward facing spike
Author:
Publisher
Elsevier BV
Subject
General Engineering,General Computer Science
Reference14 articles.
1. Unsteady aerodynamic considerations in the design of a drag reduction spike;Reding;Journal of Spacecraft and Rockets,1977
2. Experiments on separation on boundary layers on probes in front of blunt-nosed bodies in supersonic air stream;Mair;Philosophical Magazine,1952
3. Preliminary investigations of spiked bodies at hypersonic speeds;Bogdonoff;Journal of Aeronautical Sciences,1959
4. Effect of a spike on the drag and on the aerodynamic stability of blunt bodies in supersonic flow;Zorea;Journal of Spacecraft and Rockets,1990
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1. Drag Reduction of a Hemispherical Body Adopting Spike at Supersonic Speed;Journal of Aerospace Sciences and Technologies;2023-08-15
2. Supersonic flow investigation of a drag reducing conical spike on a hemispherically blunted nose body;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-11-26
3. Thermo-Fluid Analysis of Supersonic Flow Over Ballistic Shaped Bodies with multiple aero-disk spike configurations;Acta Astronautica;2021-03
4. Drag reduction for payload fairing of satellite launch vehicle with aerospike in transonic and low supersonic speeds;ADV AIRCR SPACECR SC;2020
5. Reduction of wave drag on parameterized blunt bodies using spikes with varied tip geometries;Acta Astronautica;2019-07
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