Pressure and its derivative with respect to piston Mach number for an oscillating cone
The aim of present study is to obtain mathematical expressions for surface pressure and its derivative with respect to Piston Mach number for an oscillating cone. The effects of Mach number and it’s geometry on Pressure and its derivative with respect to inertia level and incidence angle, and the re...
Main Authors: | Shabana, Ayesha, Monis, Renita, Crasta, Asha, Khan, Sher Afghan |
---|---|
Format: | Article |
Language: | English |
Published: |
International Organization of Scientific Research ( IOSR )
2016
|
Subjects: | |
Online Access: | http://irep.iium.edu.my/54290/ http://irep.iium.edu.my/54290/ http://irep.iium.edu.my/54290/ http://irep.iium.edu.my/54290/1/Ayesha.pdf |
Similar Items
-
Active control of wall pressure flow field at low supersonic Mach numbers
by: Asad Ullah, Mohammed, et al.
Published: (2016) -
Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
by: Crasta, Asha, et al.
Published: (2012) -
Base pressure behaviour in a suddenly expanded duct at supersonic mach number regimes using Taguchi design of experiments
by: Quadros, Jaimon Dennis, et al.
Published: (2018) -
Role of active control in increasing base pressure at Sonic Mach Number
by: G. M, Fharukh Ahmed, et al.
Published: (2019) -
Experimental research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24
by: Khan, Sher Afghan, et al.
Published: (2019)