Vasishta Bhargava

Sreyas Institute of Engineering and Technology

Hyderabad-500065

Telangana

India

SCHOLARLY PAPERS

6

DOWNLOADS

183

CITATIONS

1

Ideas:
“  1. Computational Aeroacoustics of slender bluff body structures2. Aerodynamic characterization of multielement aerofoils for low Re flows3. Experimental flow visualization methods of rotating wing structures for high Reynolds number flows  ”

Scholarly Papers (6)

1.

Computational Analysis of NACA 0010 at Moderate to High Reynolds Number Using 2D Panel Method

International Conference on Advances in Thermal Systems, Materials and Design Engineering (ATSMDE2017)
Number of pages: 8 Posted: 19 Jan 2018
Vasishta Bhargava, M Satya Prasad and Md Ahkar Khan
Sreyas Institute of Engineering and Technology, GITAM University, Visakhapatnam - Gandhi Institute of Technology and Management (GITAM) and GITAM University, Visakhapatnam - Gandhi Institute of Technology and Management (GITAM)
Downloads 64 (343,133)

Abstract:

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Airfoil, Panel method, Pressure coefficient, Angle of attack, Chord

2.

Prediction of Aerodynamic Characteristics for Slender Bluff Bodies with Different Nose Cone Shapes

Number of pages: 11 Posted: 27 Feb 2018
Y D Dwivedi and Vasishta Bhargava
Vignan's Foundation for Science, Technology & Research (VFSTR) University and Sreyas Institute of Engineering and Technology
Downloads 47 (396,103)

Abstract:

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Method, Nosecone, Coefficient of Lift, Coefficient of Drag, Pressure Distribution, Angle of Attack

3.

Trailing Edge Noise Prediction from NaACA 0012 & NACA 6320 Using Empirical Pressure Spectrum Models

IOSR Journal of Applied Physics (IOSR-JAP), e-ISSN: 2278-4861. Volume 10, Issue 2, Ver. I (Mar. – Apr. 2018), Pp. 33-46
Number of pages: 14 Posted: 23 Apr 2018
Vasishta Bhargava, S. Rahul and HimaBindu Venigalla
Sreyas Institute of Engineering and Technology, Indian Institute of Technology (IIT), Chennai and GITAM University, Visakhapatnam - Department of Aerospace Engineering
Downloads 28 (474,261)

Abstract:

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Airfoil, Noise, Sound Pressure Level, Trailing edge, Boundary layer

4.

Aero-Acoustic Analysis of Wind Turbines: Turbulent Boundary Layer Trailing Edge Noise

International Journal of Innovations in Engineering and Technology (IJIET), Volume 8 Issue 1-February 2017
Number of pages: 10 Posted: 23 Apr 2018
Vasishta Bhargava, HimaBindu Venigalla and Y.D. Dwivedi
Sreyas Institute of Engineering and Technology, GITAM University, Visakhapatnam - Department of Aerospace Engineering and GITAM University, Visakhapatnam - Department of Aeronautical Engineering
Downloads 24 (495,722)

Abstract:

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Sound pressure level, Airfoil, Boundary layer, Angle of Attack, Directivity, Reynolds number, Strouhal number, Mach number, Center frequency

5.

A Review of Trailing Edge Bluntness and Tip Noise Mechanism from Wind Turbine Blades

IOSR Journal of Applied Physics (IOSR-JAP), e-ISSN: 2278-4861. Volume 9, Issue 4, Ver. IV (Jul. – Aug. 2017), Pp. 20-31
Number of pages: 13 Posted: 23 Apr 2018
Vasishta Bhargava, HimaBindu Venigalla and J.V. Ramakanth
Sreyas Institute of Engineering and Technology, GITAM University, Visakhapatnam - Department of Aerospace Engineering and Sreyas Institute of Engineering and Technology - Department of Mechanical Engineering
Downloads 12 (565,995)

Abstract:

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Airfoil, Boundary layer, Sound power level, Reynolds number, Mach number, Wind turbine

6.

BEM Prediction of Wind Turbine Operation and Performance

INTERNATIONAL JOURNAL of RENEWABLE ENERGY RESEARCH, Vol.8, No.4, 2018
Number of pages: 12 Posted: 10 May 2019
Jaya M. Krishna, Vasishta Bhargava and Jagadeesh Donepudi
GITAM University, Visakhapatnam - Gandhi Institute of Technology and Management (GITAM), Sreyas Institute of Engineering and Technology and Narasaraopeta Engineering College - Department of Mechanical Engineering
Downloads 8 (590,984)

Abstract:

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Wind turbine, Thrust, BEM, Torque, Power, Wind Speed, Angle of attack