Ministry of Education
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Dr Dileepkumar Bhanudasji Alone

vidwan id: 69093
Male

Senior Principal Scientist, Propulsion Division
CSIR-National Aerospace Laboratories

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Expertise

  • Aerospace Engineering

Publications

Total Articles 21
Books 0
Proceedings 0

Publications

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Scopus

Citations 93
h-index 5

CrossRef

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Citations 43
h-index 4
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Bio

Mechanical Engg,Jet Propulsion and Gas Turbine,Operation Research, Axial Flow Compressor Aerodynamics and Stability Management

Personal Details

  • Male
  • Senior Principal Scientist , CSIR-National Aerospace Laboratories
  • CSIR-National Aerospace Laboratories
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Senior Principal Scientist Dec 2018 – Present
CSIR-National Aerospace Laboratories | Propulsion Division
Scientist Dec 2001 – Dec 2018
CSIR-National Aerospace Laboratories | Propulsion Division

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Organisations (387+)

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Ashoka

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Technical Officer

Buddhadeb

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Scientist

Balaji

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Aruna

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Senior Principal Scientist

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Arun

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K.N.

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Arvind Kumar

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Selvamani

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Principal Technical Officer

Co-Authors (10)

A M

Dr A M Pradeep

Indian Institute of Technology Bombay

Ranjan

Prof Ranjan Ganguli

Indian Institute of Science Bangalore

S. B.

Dr S. B. Kandagal

Indian Institute of Science Bangalore

Lakshya

Mr Lakshya Kumar

CSIR-National Aerospace Laboratories

Chetankumar

Dr Chetankumar Mistry

Indian Institute of Technology Kharagpur

Shobhavathy

Ms Shobhavathy M.T

CSIR-National Aerospace Laboratories

Pramod

Dr Pramod Kumar

Indian Institute of Science Bangalore

Senthil Kumaran

Mr Senthil Kumaran Raju

CSIR-National Aerospace Laboratories

Sarat

Dr Sarat Maharana

M S Ramaiah University of Applied Sciences

Venkat Iyengar

Dr Venkat Iyengar S

CSIR-National Aerospace Laboratories

Scholarly Work

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Scholarly Publications

Aeroelastic Aspects of Axial Compressor Stage With Self-Recirculating Casing Treatment

Open Access
Article
Journal of Turbomachinery. Year: 2022. Volume: 144 , Issue: 6 .
Authors: Satish Kumar S.;Alone D.B.;Thimmaiah S.M.;Mudipalli J.R.R.;Kumar L.;Jana S.;Kandagal S.B.;Ganguli R.
DOI 10.1115/1.4053385
9 13

PRELIMINARY AERODYNAMIC DESIGN of A S-CO2 AXIAL TURBINE

Open Access
Conference Paper
Year: 2021.
Authors: Kumaran R.S.;Alone D.B.;Nassar A.;Kumar P.
DOI 10.1115/GTINDIA2021-76454
1 2

Understanding of an effect of plenum volume of a low porosity bend skewed casing treatment on the performance of single-stage transonic axial flow compressor

Open Access
Conference Paper
Year: 2021. Pages: 3-26 .
Authors: Pitroda D.P.;Alone D.B.;Choksi H.S.
DOI 10.1007/978-981-15-5039-3_1

Profile loss investigations with a S-CO2 axial turbine aerofoil

Open Access
Conference Paper
Year: 2020. Volume: 11 .
Authors: Senthil Kumaran R.;Alone D.B.;Kumar P.
DOI 10.1115/GT2020-15651
1 4

Flow studies on a single stage transonic axial flow compressor retrofitted with circumferential grooves and varied rotor-stator axial gap

Open Access
Conference Paper
Year: 2017. Volume: 1 .
Authors: Darji A.P.;Alone D.B.;Mistry C.S.
DOI 10.1115/GTINDIA2017-4592

Numerical investigations on influence of uniform blade surface roughness on the performance characteristics of a transonic axial flow compressor stage

Open Access
Conference Paper
Year: 2017. Volume: 1 .
Authors: Chotalia R.J.;Alone D.B.
DOI 10.1115/GTINDIA2017-4594
1

Experimental assessment on effect of lower porosities of bend skewed casing treatment on the performance of high speed compressor stage with tip critical rotor characteristics

Open Access
Article
Aerospace Science and Technology. Year: 2017. Volume: 60 , Pages: 193-202 .
Authors: Alone D.B.;Kumar S.S.;Shobhavathy M.T.;Mudipalli J.R.R.;Pradeep A.M.;Ramamurthy S.;Iyengar V.S.
DOI 10.1016/j.ast.2016.11.006
13 28

Stability management of high speed axial flow compressor stage through axial extensions of bend skewed casing treatment

Open Access
Article
Propulsion and Power Research. Year: 2016. Volume: 5 , Issue: 3 , Pages: 236-249 .
Authors: Alone D.B.;Kumar S.S.;Thimmaiah S.M.;Mudipalli J.R.R.;Pradeep A.M.;Ramamurthy S.;Iyengar V.S.
DOI 10.1016/j.jppr.2016.01.009
5 14