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: Bashir, Musavir, Khan, Sher Afghan, Azam, Qummare, Janvekar, Ayub
Format: Article
Language:English
English
Published: Faculty of Engineering, Universitas Indonesia 2017
Subjects:
Online Access:http://irep.iium.edu.my/56874/13/56874_COMPUTATIONAL%20AND%20ANALYTICAL%20INVESTIGATION_article.pdf
http://irep.iium.edu.my/56874/7/56874_Computational%20and%20analytical%20investigation_SCOPUS.pdf
http://irep.iium.edu.my/56874/
http://ijtech.eng.ui.ac.id/article/view/176
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