Inspection of supersonic flows in a CD nozzle using experimental method
In high speed flows nozzles are used to change pressure energy to kinetic energy which in turn is used to produce thrust. In a converging-diverging nozzle, flow is augmented from subsonic to sonic velocity at the throat and further expanded to supersonic velocities at the exit. In this paper, an exp...
Main Authors: | Azami, Muhammad Hanafi, Faheem, Mohammed, Aabid, Abdul, Mokashi, Imran, Khan, Sher Afghan |
---|---|
Format: | Article |
Language: | English English |
Published: |
2019
|
Subjects: | |
Online Access: | http://irep.iium.edu.my/74320/ http://irep.iium.edu.my/74320/ http://irep.iium.edu.my/74320/1/IJRTE%20Nozzle%20Paper.pdf http://irep.iium.edu.my/74320/7/74320_Inspection%20of%20supersonic%20flows%20in%20a%20CD%20nozzle%20using%20experimental%20method_Scopus.pdf |
Similar Items
-
Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5
by: Azami, Muhammad Hanafi, et al.
Published: (2019) -
Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow
by: Bashir, Musavir, et al.
Published: (2015) -
Control of nozzle flow using microjets at supersonic Mach Regime
by: G M, Fharukh, et al.
Published: (2019) -
Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2016) -
CFD analysis of CD nozzle and effect of nozzle pressure ratio on pressure and velocity for suddenly expanded flows
by: Khan, Sher Afghan, et al.
Published: (2018)