compressible jet Latest Research Papers

Study of multi-mode forcing effects on coherent structures of flow transition in a compressible jet

AIP Advances ◽

10.1063/5.0067533 ◽

2021 ◽

Vol 11 (11) ◽

pp. 115105

Author(s):

Cong Xu ◽

Huanxin Lai

Keyword(s):

Coherent Structures ◽

Flow Transition ◽

Multi Mode ◽

Compressible Jet

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Correlation in the Near and Far Field of Compressible Jet to Identify Noise Source Characteristics

Flow Turbulence and Combustion ◽

10.1007/s10494-021-00299-2 ◽

2021 ◽

Author(s):

Shailesh Ravindra Nikam ◽

Shailendra Sharma

Keyword(s):

Noise Source ◽

Far Field ◽

Source Characteristics ◽

Compressible Jet

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Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due to Chevron

Lecture Notes in Mechanical Engineering - Design and Development of Aerospace Vehicles and Propulsion Systems ◽

10.1007/978-981-15-9601-8_1 ◽

2021 ◽

pp. 1-13

Author(s):

S. R. Nikam ◽

S. D. Sharma

Keyword(s):

Mach Number ◽

Compressible Jet

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Noise Source Characteristics of Compressible Jet from Non-axisymmetric Nozzles

Lecture Notes in Mechanical Engineering - Proceedings of 16th Asian Congress of Fluid Mechanics ◽

10.1007/978-981-15-5183-3_39 ◽

2021 ◽

pp. 363-373

Author(s):

Shailesh R. Nikam ◽

Siddhesh Bhikole ◽

Malay Suvagiya

Keyword(s):

Noise Source ◽

Source Characteristics ◽

Compressible Jet

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Preliminary Studies of Compressible Jet Flow from a Pipe with Hexagonal Cross-section

IOP Conference Series Materials Science and Engineering ◽

10.1088/1757-899x/912/4/042057 ◽

2020 ◽

Vol 912 ◽

pp. 042057

Author(s):

S Avinash ◽

K Tinesh ◽

B T Kannan

Keyword(s):

Cross Section ◽

Jet Flow ◽

Hexagonal Cross Section ◽

Compressible Jet

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Preliminary Studies on Compressible Jet Flow from a Pipe with Square Cross-section

IOP Conference Series Materials Science and Engineering ◽

10.1088/1757-899x/912/4/042058 ◽

2020 ◽

Vol 912 ◽

pp. 042058

Author(s):

K Tinesh ◽

S Avinash ◽

B T Kannan

Keyword(s):

Cross Section ◽

Jet Flow ◽

Compressible Jet

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Wall-Pressure Fluctuations Induced by a Compressible Jet in Installed Configuration

AIAA Journal ◽

10.2514/1.j058791 ◽

2020 ◽

Vol 58 (7) ◽

pp. 2991-3000 ◽

Cited By ~ 3

Author(s):

Stefano Meloni ◽

Matteo Mancinelli ◽

Roberto Camussi ◽

Jérôme Huber

Keyword(s):

Pressure Fluctuations ◽

Wall Pressure ◽

Wall Pressure Fluctuations ◽

Compressible Jet

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Numerical simulation of a supersonic turbulent compressible jet in a co-flow with stochastic spectral inflow boundary conditions

International Journal of Mathematics and Physics ◽

10.26577/ijmph.2020.v11.i1.03 ◽

2020 ◽

Vol 11 (1) ◽

pp. 20-27

Author(s):

A. Zadauly ◽

◽

A. O. Beketaeva ◽

Keyword(s):

Numerical Simulation ◽

Boundary Conditions ◽

Compressible Jet

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Withdrawal: Azimuthal variation of Near Field Pressure Fluctuations due to Chevron in Compressible Jet

25th AIAA/CEAS Aeroacoustics Conference ◽

10.2514/6.2019-2434.c1 ◽

2019 ◽

Author(s):

Shailesh R. Nikam ◽

Shailendra Sharma

Keyword(s):

Near Field ◽

Pressure Fluctuations ◽

Azimuthal Variation ◽

Compressible Jet

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Withdrawal: Acoustic Characteristics of Compressible Jet from Different Nozzle exit Geometry

25th AIAA/CEAS Aeroacoustics Conference ◽

10.2514/6.2019-2595.c1 ◽

2019 ◽

Author(s):

Shailesh R. Nikam ◽

Siddhesh Bhikole ◽

Malay Suvagiya

Keyword(s):

Nozzle Exit ◽

Acoustic Characteristics ◽

Compressible Jet

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compressible jet
Recently Published Documents

TOTAL DOCUMENTS

H-INDEX

Study of multi-mode forcing effects on coherent structures of flow transition in a compressible jet

Correlation in the Near and Far Field of Compressible Jet to Identify Noise Source Characteristics

Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due to Chevron

Noise Source Characteristics of Compressible Jet from Non-axisymmetric Nozzles

Preliminary Studies of Compressible Jet Flow from a Pipe with Hexagonal Cross-section

Preliminary Studies on Compressible Jet Flow from a Pipe with Square Cross-section

Wall-Pressure Fluctuations Induced by a Compressible Jet in Installed Configuration

Numerical simulation of a supersonic turbulent compressible jet in a co-flow with stochastic spectral inflow boundary conditions

Withdrawal: Azimuthal variation of Near Field Pressure Fluctuations due to Chevron in Compressible Jet

Withdrawal: Acoustic Characteristics of Compressible Jet from Different Nozzle exit Geometry

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compressible jetRecently Published Documents

TOTAL DOCUMENTS

H-INDEX

Study of multi-mode forcing effects on coherent structures of flow transition in a compressible jet

Correlation in the Near and Far Field of Compressible Jet to Identify Noise Source Characteristics

Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due to Chevron

Noise Source Characteristics of Compressible Jet from Non-axisymmetric Nozzles

Preliminary Studies of Compressible Jet Flow from a Pipe with Hexagonal Cross-section

Preliminary Studies on Compressible Jet Flow from a Pipe with Square Cross-section

Wall-Pressure Fluctuations Induced by a Compressible Jet in Installed Configuration

Numerical simulation of a supersonic turbulent compressible jet in a co-flow with stochastic spectral inflow boundary conditions

Withdrawal: Azimuthal variation of Near Field Pressure Fluctuations due to Chevron in Compressible Jet

Withdrawal: Acoustic Characteristics of Compressible Jet from Different Nozzle exit Geometry

compressible jet
Recently Published Documents