Khoiri Rozi
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Khoiri Rozi has a total of 7 co-authors. Here are the top co-authors by number of shared publications:
- Agus Suprihanto
Diponegoro University
1 shared publication - Azwinur Azwinur1 shared publication
- Mohammad Reza Kariman
Institute for Energy Systems and Thermodynamics, TU Wien, Getreidemarkt 9, A-1060 Vienna, Austria
1 shared publication Mukhsinun Hadi Kusuma
1 shared publication- Reinhard Willinger
Institute for Energy Systems and Thermodynamics, TU Wien, Getreidemarkt 9, A-1060 Vienna, Austria
1 shared publication - Surya Dharma
Program Studi Teknik Mesin, Jurusan Teknik Mesin, Politeknik Negeri Medan, Jl. Almamater No.1, Padang Bulan, Kec. Medan Baru, Kota medan, Sumatera Utara 20155, Indonesia
1 shared publication
Latest Publications
- Open Access
- 1 May 2026
- Published by WNGB Scientific Publishing House Sp. z o.o. in Advances in Science and Technology Research Journal
- Vol. 20 (5) , 171-184
Thermo-mechanical behavior of Cu/SS316L dissimilar welded joints for heat pipe applications
Dissimilar welding between copper (Cu) and stainless steel 316L (SS316L) is essential for heat pipe applications that require high thermal conductivity combined with adequate mechanical integrity. However, the large mismatch in thermal and metallurgical properties between Cu and SS316L...
- 1 May 2026
- Published by WNGB Scientific Publishing House Sp. z o.o. in Advances in Science and Technology Research Journal
- Vol. 20 (5) , 171-184
Open AccessThermo-mechanical behavior of Cu/SS316L dissimilar welded joints for heat pipe applications
Dissimilar welding between copper (Cu) and stainless steel 316L (SS316L) is essential for heat pipe applications that require high thermal conductivity combined with adequate mechanical integrity. However, the large mismatch in thermal and metallurgical properties between Cu and SS316L...
- Open Access
- 2 March 2026
- Published by MDPI AG in International Journal of Turbomachinery, Propulsion and Power
- Vol. 11 (1) , 13
Two-Dimensional Flow in a Linear Cascade of Throttling Nozzles for an Adaptive Turbine Stage
Steam turbines with controlled extraction require a flow control device to keep extraction pressure constant when the extraction mass flow rate is changed. An attractive option is an adaptive turbine stage with throttling nozzles. Flow measurements with a throttling nozzle are performed in a cascade wind tunnel. A linear cascade with seven blades is operated at an inlet flow angle of 90° and an exit Reynolds number of about 4 × 105. Since the maximum exit Mach number is about 0.2, flow is essentially incompressible. A three-hole pressure probe is traversed at half span over one blade pitch 0.33 axial chord lengths downstream of the cascade. Degree of closing is gradually changed from zero (fully open) to 0.3 (partially closed). Two principal options, closing to the suction side as well as closing to the pressure side, are investigated. Local flow quantities as well as pitchwise mass averaged quantities are extracted from the measurement data. The major outcomes are as follows: If the throttling nozzle is closed, depth and width of the blade wake increase. With increasing degree of closing, pitchwise mass averaged flow angle decreases and total pressure losses increase. Concerning total pressure losses, closing to the pressure side is the preferred option. A semi-empirical flow model is presented to explain the influence of degree of closing on exit flow angle and total pressure loss.
- 2 March 2026
- Published by MDPI AG in International Journal of Turbomachinery, Propulsion and Power
- Vol. 11 (1) , 13
Open AccessTwo-Dimensional Flow in a Linear Cascade of Throttling Nozzles for an Adaptive Turbine Stage
Steam turbines with controlled extraction require a flow control device to keep extraction pressure constant when the extraction mass flow rate is changed. An attractive option is an adaptive turbine stage with throttling nozzles. Flow measurements with a throttling nozzle are performed in a cascade wind tunnel. A linear cascade with seven blades is operated at an inlet flow angle of 90° and an exit Reynolds number of about 4 × 105. Since the maximum exit Mach number is about 0.2, flow is essentially incompressible. A three-hole pressure probe is traversed at half span over one blade pitch 0.33 axial chord lengths downstream of the cascade. Degree of closing is gradually changed from zero (fully open) to 0.3 (partially closed). Two principal options, closing to the suction side as well as closing to the pressure side, are investigated. Local flow quantities as well as pitchwise mass averaged quantities are extracted from the measurement data. The major outcomes are as follows: If the throttling nozzle is closed, depth and width of the blade wake increase. With increasing degree of closing, pitchwise mass averaged flow angle decreases and total pressure losses increase. Concerning total pressure losses, closing to the pressure side is the preferred option. A semi-empirical flow model is presented to explain the influence of degree of closing on exit flow angle and total pressure loss.