RTU Research Outputs and Resources: Reasearch Staff

Information about Author

Name, Surname:

Ali Arshad

Department:

(25100) Aeronautikas institūts

Scientific Degree:

Doktors

E-mail:

Ali.Arshad(at)rtu.lv

Publications

20 items found, displaying 11 to 20.

A Simplified Design Approach for High-Speed Wind Tunnels. Part I: Table of Iclination
(2020)

Ali Arshad, S. Samarasinghe, F.A.M. Akeel, Aleksandrs Urbahs
Scientific article indexed in SCOPUS or WOS database

A Simplified Design Approach for High-Speed Wind Tunnels. Part-I.I: Optimized Design of Settling Chamber and Inlet Nozzle
(2020)

Ali Arshad, Supun Samarasinghe, Vadims Kovalcuks
Full-text conference paper published in conference proceedings indexed in SCOPUS or WOS database

Computational Study of Noise Reduction in CFM56-5B Using Core Nozzle Chevrons
(2020)

Ali Arshad, Naveen Ansdrew, Ilmārs Blumbergs
Full-text conference paper published in conference proceedings indexed in SCOPUS or WOS database

Effects of Inlet Radial Distortion on the Type of Stall Precursor in Low-Speed Axial Compressor
(2018)

Ali Arshad, Qiushi Li, Simin Li, Tianyu Pan
Scientific article indexed in SCOPUS or WOS database

Comparison of Different Stall Conditions in Axial Flow Compressor Using Analytic Wavelet Transform
(2017)

Ali Arshad, Li Qiushi
Publication (anonimusly reviewed) in a journal with an international editorial board indexed in other databases

Effects of Increasing Blade Hub Loading on Instability Evolution in a Low-Speed Compressor
(2017)

Qiushi Li, Simin Li, Tianyu Pan, Ali Arshad, Yifang Gong
Full-text conference paper published in conference proceedings indexed in SCOPUS or WOS database

Application of Non Filtering Analytic Wavelet Transform for the Investigation of Rotating Stall Inception in Low Speed Compressor
(2016)

Ali Arshad, Qiushi Li, Tianyu Pan
Full-text conference paper published in conference proceedings indexed in SCOPUS or WOS database

The Mechanism of Propagation of Tip Clearance Flow and Corner Separation in High Temperature Silicon Based Micro Compressor
(2015)

Ali Arshad, Qianwei Sun, Qiushi Li
Full-text conference paper published in conference proceedings indexed in SCOPUS or WOS database

Non-Adiabatic Flow Characteristics of Micro Impeller
(2014)

Qianwei Sun, Qiushi Li, Ali Arshad, Zhiping Li
Scientific article indexed in SCOPUS or WOS database

A Flow Visualization and Aerodynamic Force Measurement of Non-Slender Delta Wing
(2011)

Saifur Rahman Bakaul, Ali Arshad, Muhammad Yamin Younis
Full-text conference paper published in other conference proceedings

Patents

1 items found, displaying 1 to 1.

Supersonic wind tunnel with a new convergent section for the inlet nozzle
LV15658B (20.01.2023.)

Ali Arshad

Projects

3 items found, displaying 1 to 3.

Aeronautikas institūts (13-25100-C3828)

Ali Arshad

Aeronautikas tehnoloģiju katedra (13-25101-90)
Citi

Margarita Urbaha

Inovatīva virsskaņas aerodinamiskā tuneļa un aerokosmisku objektu īpašību izpētes metodoloģijas izstrāde
Citi

Margarita Urbaha

Information about Author

Publications

A Simplified Design Approach for High-Speed Wind Tunnels. Part I: Table of Iclination (2020)

A Simplified Design Approach for High-Speed Wind Tunnels. Part-I.I: Optimized Design of Settling Chamber and Inlet Nozzle (2020)

Computational Study of Noise Reduction in CFM56-5B Using Core Nozzle Chevrons (2020)

Effects of Inlet Radial Distortion on the Type of Stall Precursor in Low-Speed Axial Compressor (2018)

Comparison of Different Stall Conditions in Axial Flow Compressor Using Analytic Wavelet Transform (2017)

Effects of Increasing Blade Hub Loading on Instability Evolution in a Low-Speed Compressor (2017)

Application of Non Filtering Analytic Wavelet Transform for the Investigation of Rotating Stall Inception in Low Speed Compressor (2016)

The Mechanism of Propagation of Tip Clearance Flow and Corner Separation in High Temperature Silicon Based Micro Compressor (2015)

Non-Adiabatic Flow Characteristics of Micro Impeller (2014)

A Flow Visualization and Aerodynamic Force Measurement of Non-Slender Delta Wing (2011)

Patents

Supersonic wind tunnel with a new convergent section for the inlet nozzle LV15658B (20.01.2023.)

Projects

Aeronautikas institūts (13-25100-C3828)

Aeronautikas tehnoloģiju katedra (13-25101-90) Citi

Inovatīva virsskaņas aerodinamiskā tuneļa un aerokosmisku objektu īpašību izpētes metodoloģijas izstrāde Citi

A Simplified Design Approach for High-Speed Wind Tunnels. Part I: Table of Iclination
(2020)

A Simplified Design Approach for High-Speed Wind Tunnels. Part-I.I: Optimized Design of Settling Chamber and Inlet Nozzle
(2020)

Computational Study of Noise Reduction in CFM56-5B Using Core Nozzle Chevrons
(2020)

Effects of Inlet Radial Distortion on the Type of Stall Precursor in Low-Speed Axial Compressor
(2018)

Comparison of Different Stall Conditions in Axial Flow Compressor Using Analytic Wavelet Transform
(2017)

Effects of Increasing Blade Hub Loading on Instability Evolution in a Low-Speed Compressor
(2017)

Application of Non Filtering Analytic Wavelet Transform for the Investigation of Rotating Stall Inception in Low Speed Compressor
(2016)

The Mechanism of Propagation of Tip Clearance Flow and Corner Separation in High Temperature Silicon Based Micro Compressor
(2015)

Non-Adiabatic Flow Characteristics of Micro Impeller
(2014)

A Flow Visualization and Aerodynamic Force Measurement of Non-Slender Delta Wing
(2011)

Supersonic wind tunnel with a new convergent section for the inlet nozzle
LV15658B (20.01.2023.)

Aeronautikas tehnoloģiju katedra (13-25101-90)
Citi

Inovatīva virsskaņas aerodinamiskā tuneļa un aerokosmisku objektu īpašību izpētes metodoloģijas izstrāde
Citi