表紙画像

Experimental study of midplane jet evolution in multiple jets at Mach 2.0

The flowfield characteristics are experimentally studied in the inter-nozzle region of free jets from twin and triple supersonic nozzles. The nozzle is designed for Mach number 2.0, and the inter-nozzle spacing is twice the nozzle exit diameter. The impact of multiple jets on the flow characteristic...

保存先:

書誌詳細
主要な著者:	Faheem, Mohammed, Khan, Aqib, Kumar, Rakesh, Khan, Sher Afghan, Asrar, Waqar, Sapardi, Mohd Azan Mohammed
フォーマット:	Conference or Workshop Item
言語:	English English English
出版事項:	Elsevier Ltd 2021
主題:	TL500 Aeronautics
オンライン･アクセス:	http://irep.iium.edu.my/92646/7/92646_Experimental%20study%20of%20midplane%20jet_SCOPUS.pdf http://irep.iium.edu.my/92646/8/92646_Experimental%20study%20of%20midplane%20jet.pdf http://irep.iium.edu.my/92646/9/92646_Experimental%20study%20of%20midplane%20jet_WoS.pdf http://irep.iium.edu.my/92646/ https://www.journals.elsevier.com/materials-today-proceedings https://doi.org/10.1016/j.matpr.2021.02.362
タグ:	タグ追加タグなし, このレコードへの初めてのタグを付けませんか!

類似資料

Estimation of Mach numbers in supersonic jets using schlieren images
著者:: Faheem, Mohammed, 等
出版事項: (2021)

Experimental investigation of the effect of cross wire on the flow field of elliptic jet
著者:: Faheem, Mohammed, 等
出版事項: (2021)

Experimental study on the mean flow characteristics of a supersonic multiple jet configuration
著者:: Faheem, Mohammed, 等
出版事項: (2021)

Influence of micro jets on the flow development in the enlarged duct at supersonic Mach number
著者:: Khan, Sher Afghan, 等
出版事項: (2019)

Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5
著者:: Azami, Muhammad Hanafi, 等
出版事項: (2019)

Control of suddenly expanded flows with micro-jets
著者:: Khan, Sher Afghan, 等
出版事項: (2003)

Control of base flows with micro jets
著者:: Ahmed Ali Baig, Maughal, 等
出版事項: (2011)

Studies on wall pressure flow control by micro jets for high area ratio
著者:: Ashfaq, Syed, 等
出版事項: (2014)

Control of base pressure with micro jets for area ratio 2.4
著者:: Ashfaq, Syed, 等
出版事項: (2014)

Passive control of base pressure and the flow development in a duct with sudden expansion at sonic Mach number
著者:: Zuraidi, Nur Husnina Muhamad, 等
出版事項: (2024)

Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field
著者:: Ashfaq, Syed, 等
出版事項: (2014)

Control of base flows with micro jet for area ratio of 6.25
著者:: Ali Baig, Maughal Ahmed, 等
出版事項: (2012)

Experimental studies of the base flow from the nozzles with sudden expansion with micro jets
著者:: Chaudhary, Zakir Ilahi, 等
出版事項: (2016)

Experimental investigation of a vertical round free turbulent jet
著者:: Zayan, Jalal Mohammad, 等
出版事項: (2013)

Effectiveness of micro-jets at different level of expansion
著者:: Chaudhary, Zakir Ilahi, 等
出版事項: (2015)

Influence of microjets on flow development at supersonic mach numbers with sudden expansion
著者:: Delvi, Hamza Afser, 等
出版事項: (2021)

Effect of micro jet control on the flow filed of the duct at Mach 1.5
著者:: Khan, Sher Afghan, 等
出版事項: (2019)

Control of nozzle flow in a suddenly expanded duct with micro jets
著者:: Baig, Maugal Ahmed Ali, 等
出版事項: (2012)

Effects of micro jets on the flow field of the duct with sudden expansion
著者:: Akhtar, Mohammad Nishat, 等
出版事項: (2019)

Development of a jet powered floating platform (in air)
著者:: Zharif, M., 等
出版事項: (2011)

Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24
著者:: Anuar, Farhana Nur Danisyah Mohd Anuar, 等
出版事項: (2024)

Regression analysis of flow parameters at high Mach numbers
著者:: Al-Khalifah, Turki, 等
出版事項: (2020)

Effect of mach number on wall pressure flow field for area ratio 2.56
著者:: Ashfaq, Syed, 等
出版事項: (2014)

Effect of mach number on stiffness and damping derivatives for oscillating hyersonic non-planar wedge
著者:: Crasta, Asha, 等
出版事項: (2014)

Studies on flows development in a suddenly expanded circular duct at supersonic mach numbers
著者:: Aabid, Abdul, 等
出版事項: (2021)

Base pressure control by supersonic micro jets in a suddenly expanded nozzle
著者:: Khan, Sher Afghan, 等
出版事項: (2018)

Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers
著者:: Pathan, Khizer Ahmed, 等
出版事項: (2018)

Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number
著者:: Renita, sharon Monis, 等
出版事項: (2020)

Prediction of base pressure in a suddenly expanded flow the processes at supersonic Mach Number Regimes using ANN and CFD
著者:: Quadros, Jaimon Dennis, 等
出版事項: (2020)

Numerical simulation of suddenly expanded flow at Mach 2.2
著者:: Aabid, Abdul, 等
出版事項: (2019)

Active control of base pressure with counter clockwise rotating cylinder at Mach 2
著者:: Asadullah, Mohammed, 等
出版事項: (2018)

Numerical simulation of surface pressure of a wedge at supersonic Mach numbers and application of design of experiments
著者:: Shamitha, Shamitha, 等
出版事項: (2023)

Numerical simulation of surface pressure and temperature distribution along a cone at supersonic Mach numbers using CFD
著者:: Shaikh, Javed Shoukat, 等
出版事項: (2025)

Effect of sweptback angle of a delta wing on surface pressure distribution at supersonic Mach numbers
著者:: Shetty, Shamitha, 等
出版事項: (2024)

Effectiveness of cone angle on surface pressure distribution along slant length of a cone at hypersonic mach numbers
著者:: Sheikh, Javed S, 等
出版事項: (2023)

Comprehensive CFD analysis of base pressure control using quarter ribs in sudden expansion duct at sonic Mach numbers
著者:: Khan, Ambareen, 等
出版事項: (2024)

Control of suddenly expanded flow using quarter rib for area ratio 4.84 at Mach 2
著者:: Chaudhary, Zakir Ilahi, 等
出版事項: (2025)

Control of base pressure with micro jets:part-I
著者:: Rehman, Shafiqur, 等
出版事項: (2008)

Base pressure control using quarter circle rib in a suddenly expanded duct at screech prone Mach number M = 1.8
著者:: Chaudhary, Zakir Ilahi, 等
出版事項: (2025)

Large Eddy simulation of low Reynolds number flow around a NACA0015 airfoil with modified trailing edges
著者:: Hassan, Mohamed Ibren, 等
出版事項: (2023)