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Prof B Roy

vidwan id: 11231
Male

,

Expertise

  • Aerospace Engineering

Publications

Total Articles 35
Books 0
Proceedings 0

Publications

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Scopus

Citations 261
h-index 10

CrossRef

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Citations 54
h-index 4
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Professional Recognition

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Fellowship

Aeronautical Society of India

Community & Membership

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Bio

Cascade Studies of Highly Loaded, Swept, Blade Profiles for Axial Compressor/Fan, Contra-Rotating Twin Rotor Axial Flow Fans, Casing Boundary Layer Control in Axial Flow Fan/Compressor, Axial Flow Fan/Compressor Performance with Distortion and Swirl.

Personal Details

  • Male
  • Indian Institute of Technology Bombay, Powai
Ph.D
Other Institute 1984
Former Professor Jan 1996 – —
Indian Institute of Technology Bombay | Department of Aerospace Engineering

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Organisation (0)

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Co-Authors (4)

A M

Dr A M Pradeep

Indian Institute of Technology Bombay

Bhaskar

Dr Bhaskar Roy

Asansol Engineering College

Emandi

Mr Emandi Rajesh

CSIR-National Aerospace Laboratories

Ujjwal K

Prof Ujjwal K Saha

Indian Institute of Technology Guwahati

Scholarly Work

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Scholarly Publications

Investigation of turbine cascade blades with part-span sweep with an open end

Open Access
Conference Paper

Application of sweep to low pressure turbine cascade blade for tip flow containment

Open Access
Conference Paper
Authors: Trehan R.F.;Roy B.
1

Effect of rotor tip gap variation at the rear stages of an axial flow compressor

Open Access
Conference Paper

Boundary layer control in turbine exhaust diffusers using casing injection and design modifications

Open Access
Conference Paper

Effect of turbine tip leakage flows on exhaust diffuser performance

Open Access
Conference Paper
Authors: Babu M.;Bhatia D.;Shukla R.K.;Pradeep A.M.;Roy B.

Study of tip flows in high hub-to-tip ratio axial compressors at low speed with varying tip gaps, inflow conditions and tip shapes

Open Access
Conference Paper

Study of gas turbine exhaust diffuser performance and its enhancement by shape modifications

Open Access
Conference Paper

Part-span application of sweep and lean at turbine blade tips - A low speed experimental cascade study

Open Access
Conference Paper