Computational and Analytical Investigation of Aerodynamic Derivatives of Similitude Delta Wing Model at Hypersonic Speeds

Computational and Analytical Investigation of Aerodynamic Derivatives of Similitude Delta Wing Model at Hypersonic Speeds

This research paper presents a computational and analytical investigation of aerodynamic derivatives in an oscillating wedge. Unsteady hypersonic similitude has been apprehended for an oscillating wedge with an attached bow shock at a large incidence angle. The problems of instability and shock wave...

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Bibliographic Details
Main Authors: Musayir Bashir, S.A. Khan, Qummare Azam, Ayub Ahmed Janvekar
Format: Article
Language:English
Published: Universitas Indonesia 2017-04-01
Series:International Journal of Technology
Subjects:
Damping derivatives
Hypersonic flow
Piston theory
Stiffness derivatives
Wedge model
Online Access:http://ijtech.eng.ui.ac.id/article/view/176

Internet

http://ijtech.eng.ui.ac.id/article/view/176

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