Computations of the Shock Waves at Hypersonic Velocities Taken into Account the Chemical Reactions that Appear in the Air at High Temperatures

Computations of the Shock Waves at Hypersonic Velocities Taken into Account the Chemical Reactions that Appear in the Air at High Temperatures

The temperature in the nose region of a hypersonic vehicle can be extremely high, for example, reaching approximately 11 000 K at a Mach number of 36 (Apollo reentry). The bow shock wave is normal, or nearly normal, in the nose region of a blunt body, and the gas temperature behind this shock wave c...

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Bibliographic Details
Main Authors: Mihai Leonida NICULESCU, Marius Gabriel COJOCARU, Mihai Victor PRICOP, Dumitru PEPELEA
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2015-09-01
Series:INCAS Bulletin
Subjects:
Hypersonic flow
shock waves
chemical reactions
CFD
capsule reentry
Online Access:http://bulletin.incas.ro/files/niculescu_cojocaru_pricop_pepelea_vol_7_iss_3.pdf

Internet

http://bulletin.incas.ro/files/niculescu_cojocaru_pricop_pepelea_vol_7_iss_3.pdf

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