Experimental investigation on the effectiveness of active control mechanism on base pressure at low supersonic mach numbers
In the current investigation, the experiments were carried out to evaluate the effectiveness of microjets in controlling the base pressure from a convergentdivergent nozzle at low supersonic Mach at different expansion level. Tests were carried out for low supersonic Mach numbers 1.25, 1.3, 1.48, an...
Saved in:
Main Authors: | Chaudhary, Zakir Ilahi, Shinde, Vilas B., Bashir, Musavir, Khan, Sher Afghan |
---|---|
Format: | Article |
Language: | English English |
Published: |
Springer Science + Business Media
2017
|
Subjects: | |
Online Access: | http://irep.iium.edu.my/62899/1/62899_Experimental%20investigation%20on%20the%20effectiveness_article.pdf http://irep.iium.edu.my/62899/2/62899_Experimental%20investigation%20on%20the%20effectiveness_scopus.pdf http://irep.iium.edu.my/62899/ https://link.springer.com/chapter/10.1007%2F978-981-10-1771-1_24 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Control of suddenly expanded flow at low supersonic Mach
numbers
by: Chaudhury, Zakir Ilahi, et al.
Published: (2015) -
Base pressure control by supersonic micro jets in a suddenly expanded nozzle
by: Khan, Sher Afghan, et al.
Published: (2018) -
Active control of wall pressure flow field at low supersonic Mach numbers
by: Asad Ullah, Mohammed, et al.
Published: (2016) -
Response of active control on the flow field of the duct pressure at supersonic Mach numbers
by: Ridwan, R, et al.
Published: (2022) -
Wall Pressure Measurements Beneath the Supersonic Jets in
an Abruptly Augmented Nozzle
by: Bashir, Musavir, et al.
Published: (2020)