Suppression of Pressure Oscillation in Supersonic Parachute Model Using a Ring
Author:
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42405-023-00654-9.pdf
Reference15 articles.
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2. Sengupta A, Kelsch R, Roeder J, Wernet M, Witkowski A, Kandis M (2009) Supersonic performance of disk-gap-band parachutes constrained to a 0-degree trim angle. J Spacecr Rockets. https://doi.org/10.2514/1.41223
3. Xue X, Koyama H, Nakamura Y (2013) Numerical simulation of supersonic aerodynamic interaction of a parachute system. Trans Japan Soc Aeronaut Sp Sci Aerosp Technol. https://doi.org/10.2322/tastj.11.33
4. Xue XP, Koyama H, Nakamura Y, Wen CY (2015) Effects of suspension line on flow field around a supersonic parachute. Aerosp Sci Technol. https://doi.org/10.1016/j.ast.2015.02.014
5. Karagiozis K, Kamakoti R, Cirak F, Pantano C (2011) A computational study of supersonic disk-gap-band parachutes using Large-Eddy Simulation coupled to a structural membrane. J Fluids Struct. https://doi.org/10.1016/j.jfluidstructs.2010.11.007
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