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Journal Articles

CFD analysis on the effect of Pintle geometry in the performance of expansion Deflection Dual-Bell Nozzle

Atharva Naik, Samruddhi Charapalle, Yashdeep Kalekar, Gurudas Walave, K. Balaji, Dinesh Kumar Bajaj

AIP Conf. Proc. 2890, 020001 (2023)

https://doi.org/10.1063/5.0157079

Published: August 2023

View article titled, CFD analysis on the effect of Pintle geometry in the performance of expansion Deflection Dual-Bell Nozzle

Journal Articles

Study and behavior of submarine under impact loading and effective explicit dynamics analysis of black marlin glider wing torpedo

Pothuraju V. V. Satyanarayana, Vivek Sachan

AIP Conf. Proc. 2653, 020001 (2022)

https://doi.org/10.1063/5.0110757

Published: October 2022

View article titled, Study and behavior of submarine under impact loading and effective explicit dynamics analysis of black marlin glider wing torpedo

Journal Articles

On the exact solution of a singularly perturbed aerodynamic problem

Evgenii Kuznetsov, Sergey Leonov, Katherine Tsapko

AIP Conf. Proc. 2181, 020014 (2019)

https://doi.org/10.1063/1.5135674

Published: November 2019

View article titled, On the exact solution of a singularly perturbed aerodynamic problem

Journal Articles

Diffusion combustion of plane hydrogen microjet emanating from a micronozzle at subsonic and supersonic velocities

V. V. Kozlov, G. R. Grek, Yu. A. Litvinenko, A. G. Shmakov, V. V. Vikhorev

AIP Conf. Proc. 2125, 030042 (2019)

https://doi.org/10.1063/1.5117424

Published: July 2019

View article titled, Diffusion combustion of plane hydrogen microjet emanating from a micronozzle at subsonic and supersonic velocities

Journal Articles

Visualization of reacting shock wave in single pulse supersonic combustion tube

Mohammad Amri Mazlan, Mohd Yasin, Mazlan Abdul Wahid, Aminuddin Saat, Rashid Jamaludin, Ahmad Dairobi Ghazali

AIP Conf. Proc. 2062, 020055 (2019)

https://doi.org/10.1063/1.5086602

Published: January 2019

View article titled, Visualization of reacting shock wave in single pulse supersonic combustion tube

Journal Articles

Development of rotating supersonic combustion engine with swirling air-fuel injection

Ahmad Dairobi Ghazali, Mazlan Abdul Wahid, Muhammad Amri Mazlan, Aminuddin Saat, Mohd Fairus Mohd Yasin, Mizanur Rahman, Kamaruzaman Natrah, Zarhamdy Mohd Zain, Ibthisham Ardani, Adam Kasani

AIP Conf. Proc. 2062, 020036 (2019)

https://doi.org/10.1063/1.5086583

Published: January 2019

View article titled, Development of rotating supersonic combustion engine with swirling air-fuel injection

Journal Articles

Space-quality reinforced polymer-composites permitting travelling-magnetic-fields in new Indus-Hypersonic-Loop

B. N. Karkera, A. O. Surendranathan, Aayush Sinha

AIP Conf. Proc. 2057, 020029 (2019)

https://doi.org/10.1063/1.5085600

Published: January 2019

View article titled, Space-quality reinforced polymer-composites permitting travelling-magnetic-fields in new Indus-Hypersonic-Loop

Journal Articles

Dynamic derivatives assessment of earth re-entry capsule in low supersonic conditions

Dumitru Pepelea, Marius Gabriel Cojocaru, Mihai Victor Pricop, Mihai Leonida Niculescu, Mihaita Gilbert Stoican

AIP Conf. Proc. 2046, 020072 (2018)

https://doi.org/10.1063/1.5081592

Published: December 2018

View article titled, Dynamic derivatives assessment of earth re-entry capsule in low supersonic conditions

Journal Articles

Computation of the hypersonic heat flux with application to small launchers

Alexandru Iulian Onel, Alexandra Stăvărescu, Marius Gabriel Cojocaru, Mihai Victor Pricop, Mihai Leonida Niculescu, Ana-Maria Neculăescu, Tudorel-Petronel Afilipoae

AIP Conf. Proc. 2046, 020069 (2018)

https://doi.org/10.1063/1.5081589

Published: December 2018

View article titled, Computation of the hypersonic heat flux with application to small launchers

Journal Articles

Effect of pressure in crossover port to the in-cylinder flow of split-cycle engine

Firmansyah, Robert Morgan, Morgan R. Heikal, A. Rashid A. Aziz

AIP Conf. Proc. 2035, 080003 (2018)

https://doi.org/10.1063/1.5075602

Published: November 2018

View article titled, Effect of pressure in crossover port to the in-cylinder flow of split-cycle engine

Journal Articles

An effect of small angle of attack on disturbances evolution in swept wing boundary layer at Mach number M=2

N. V. Semionov, Yu. G. Yermolaev, V. L. Kocharin, A. D. Kosinov, A. N. Semenov, B. V. Smorodsky, A. A. Yatskikh

AIP Conf. Proc. 2027, 030156 (2018)

https://doi.org/10.1063/1.5065250

Published: November 2018

View article titled, An effect of small angle of attack on disturbances evolution in swept wing boundary layer at Mach number M=2

Journal Articles

Influence of gas molecular weight on jet penetration and mixing in supersonic transverse air flow in channel

N. N. Fedorova, M. A. Goldfeld, S. A. Valger

AIP Conf. Proc. 2027, 030140 (2018)

https://doi.org/10.1063/1.5065234

Published: November 2018

View article titled, Influence of gas molecular weight on jet penetration and mixing in supersonic transverse air flow in channel

Journal Articles

Methodical investigations of aerodynamic derivatives of a sharp cone on a setup with free oscillations at supersonic velocities

N. P. Adamov, A. M. Gurin, E. A. Chasovnikov

AIP Conf. Proc. 2027, 030151 (2018)

https://doi.org/10.1063/1.5065245

Published: November 2018

View article titled, Methodical investigations of aerodynamic derivatives of a sharp cone on a setup with free oscillations at supersonic velocities

Journal Articles

Self-induced oscillations of a cone with a hemispherical rear part at low supersonic velocities

N. P. Adamov, E. A. Chasovnikov

AIP Conf. Proc. 2027, 030150 (2018)

https://doi.org/10.1063/1.5065244

Published: November 2018

View article titled, Self-induced oscillations of a cone with a hemispherical rear part at low supersonic velocities

Journal Articles

On introduction of controlled disturbances into a longitudinal vortex in a supersonic boundary layer

A. Panina, A. Kosinov, N. Semionov, Yu. Yermolaev

AIP Conf. Proc. 2027, 040077 (2018)

https://doi.org/10.1063/1.5065351

Published: November 2018

View article titled, On introduction of controlled disturbances into a longitudinal vortex in a supersonic boundary layer

Journal Articles

Influence of backpressure in the combustion chamber on the characteristics of the supersonics axisymmetric air intake

D. A. Vnuchkov, V. I. Zvegintsev, D. G. Nalivaychenko, A. Yu. Melnikov, V. I. Smoljaga, A. V. Stepanov

AIP Conf. Proc. 2027, 040054 (2018)

https://doi.org/10.1063/1.5065328

Published: November 2018

View article titled, Influence of backpressure in the combustion chamber on the characteristics of the supersonics axisymmetric air intake

Journal Articles

Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability

A. D. Kosinov, N. V. Semionov, Yu. G. Yermolaev, G. L. Kolosov, A. A. Yatskikh, V. L. Kocharin

AIP Conf. Proc. 2027, 040087 (2018)

https://doi.org/10.1063/1.5065361

Published: November 2018

View article titled, Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability

Journal Articles

Experimental study of effect of a couple of weak shock waves on boundary layer of the blunt flat plate

V. L. Kocharin, N. V. Semionov, A. D. Kosinov, Yu. G. Yermolaev, A. A. Yatskikh

AIP Conf. Proc. 2027, 040026 (2018)

https://doi.org/10.1063/1.5065300

Published: November 2018

View article titled, Experimental study of effect of a couple of weak shock waves on boundary layer of the blunt flat plate

Journal Articles

Investigation of the influence of pressure redistribution arising out of the cross flow jet to the aerodynamic characteristics of the axisimmetric supersonic vehicle

V. A. Kislovskiy, V. I. Zvegintsev

AIP Conf. Proc. 2027, 040016 (2018)

https://doi.org/10.1063/1.5065290

Published: November 2018

View article titled, Investigation of the influence of pressure redistribution arising out of the cross flow jet to the aerodynamic characteristics of the axisimmetric supersonic vehicle

Journal Articles

Numerical study of unsteady effects in the interaction of an incident shock with the transitional boundary layer on a flat plate

Dmitry Khotyanovsky, Alexey Kudryavtsev

AIP Conf. Proc. 2027, 040083 (2018)

https://doi.org/10.1063/1.5065357

Published: November 2018

View article titled, Numerical study of unsteady effects in the interaction of an incident shock with the transitional boundary layer on a flat plate

NARROW

Topics

CFD analysis on the effect of Pintle geometry in the performance of expansion Deflection Dual-Bell Nozzle

Study and behavior of submarine under impact loading and effective explicit dynamics analysis of black marlin glider wing torpedo

On the exact solution of a singularly perturbed aerodynamic problem

Diffusion combustion of plane hydrogen microjet emanating from a micronozzle at subsonic and supersonic velocities

Visualization of reacting shock wave in single pulse supersonic combustion tube

Development of rotating supersonic combustion engine with swirling air-fuel injection

Space-quality reinforced polymer-composites permitting travelling-magnetic-fields in new Indus-Hypersonic-Loop

Dynamic derivatives assessment of earth re-entry capsule in low supersonic conditions

Computation of the hypersonic heat flux with application to small launchers

Effect of pressure in crossover port to the in-cylinder flow of split-cycle engine

An effect of small angle of attack on disturbances evolution in swept wing boundary layer at Mach number M=2

Influence of gas molecular weight on jet penetration and mixing in supersonic transverse air flow in channel

Methodical investigations of aerodynamic derivatives of a sharp cone on a setup with free oscillations at supersonic velocities

Self-induced oscillations of a cone with a hemispherical rear part at low supersonic velocities

On introduction of controlled disturbances into a longitudinal vortex in a supersonic boundary layer

Influence of backpressure in the combustion chamber on the characteristics of the supersonics axisymmetric air intake

Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability

Experimental study of effect of a couple of weak shock waves on boundary layer of the blunt flat plate

Investigation of the influence of pressure redistribution arising out of the cross flow jet to the aerodynamic characteristics of the axisimmetric supersonic vehicle

Numerical study of unsteady effects in the interaction of an incident shock with the transitional boundary layer on a flat plate

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