HimaBindu Venigalla

GITAM University, Visakhapatnam - Department of Aerospace Engineering

Rudraram, Mandal

Sangareddy district, Patancheru

Hyderabad, Telangana 502329

India

SCHOLARLY PAPERS

3

DOWNLOADS

62

CITATIONS

1

Scholarly Papers (3)

1.

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 27 (476,237)
Citation 1

Abstract:

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

2.

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 (492,428)

Abstract:

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

3.

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 11 (568,184)

Abstract:

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