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...
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/ http://irep.iium.edu.my/56874/ http://irep.iium.edu.my/56874/ 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 |
Similar Items
-
Hypersonic similitude for planar wedges
by: Crasta, Asha, et al.
Published: (2014) -
Estimation of stability derivatives of a delta wing in hypersonic flow
by: Crasta, Asha, et al.
Published: (2012) -
Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
by: Crasta, Asha, et al.
Published: (2012) -
Estimation of damping derivatives for delta wings in hypersonic flow for straight leading edge
by: Renita, sharon Monis, et al.
Published: (2019) -
Estimation of aerodynamic derivatives in pitch of a wedge in hypersonic flow
by: Shanbhag, Pavithra, et al.
Published: (2016)