Solution of super- and hypersonic gas dynamic problems with a model of high-temperature air

Solution of super- and hypersonic gas dynamic problems with a model of high-temperature air

The study considers the solution of a number of problems of supersonic and hypersonic gas dynamics using a model that takes into account the dissociation and ionization of air. The results of verification and validation of the developed numerical method using various difference schemes (the Roe sche...

Full description

Bibliographic Details
Main Authors:	Konstantin N. Volkov, Yuriy V. Dobrov, Anton G. Karpenko, Mikhail S. Yakovchuk
Format:	Article
Language:	English
Published:	Saint Petersburg National Research University of Information Technologies, Mechanics and Optics (ITMO University) 2021-08-01
Series:	Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki
Subjects:	mathematical modeling aerodynamics supersonic flow shock wave real gas channel
Online Access:	https://ntv.ifmo.ru/file/article/20590.pdf

Similar Items

Asymptotic solution for two-dimensional viscous supersonic and hypersonic flows past compression and expansion corners /
by: Rizzetta, Donald Pasquale
Published: (1976)

An investigation of a method for determining the pressure distribution on an accelerating flat plate at an angle of attack at hypersonic or supersonic velocities
by: Hannon, Clarence William
Published: (2006)

Aerodynamic and thermal environment of a gap under hypersonic flight
by: Huang Haiming, et al.
Published: (2018-01-01)

Grapho-analytical Analysis of Video Frames of Supersonic Flow Around Two Solid Revolutions using the Digital Image Processing Method
by: Valery V. Bodryshev, et al.
Published: (2020-05-01)

Investigation of the effects of precondensation sections in two-dimensional supersonic flow
by: McCauley, William DeForest
Published: (2006)

Numerical Study on the Aerodynamics of the Evacuated Tube Transportation System from Subsonic to Supersonic
by: Shan, X., et al.
Published: (2022)

Effect of secondary swirl in supersonic gas and plasma flows in the self-vacuuming vortex tube
by: Volov Vyacheslav, et al.
Published: (2018-01-01)

Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels
by: Vijay, B V
Published: (2012)

Discharge characteristics of a gliding arc discharge in a supersonic jet air flow
by: Feng, R., et al.
Published: (2022)

A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows
by: Davis, Jake Daniel
Published: (2019)

Numerical study on aerodynamic heat of hypersonic flight
by: Huang Haiming, et al.
Published: (2016-01-01)

The Design and Implementation of a Supersonic Indraft Tube Wind Tunnel for the Demonstration of Supersonic Flows
by: Johnson, Daniel Kenneth
Published: (2018)

Assessment of CFD Capability for Hypersonic Shock Wave Laminar Boundary Layer Interactions
by: Mehrnaz Rouhi Youssefi, et al.
Published: (2017-04-01)

Experimental Investigations on Hypersonic Waverider
by: Nagashetty, K
Published: (2018)

Hypersonic Vehicles Past, Present and Future Developments
Published: (2019)

Experimental Studies on Shock-Shock Interactions in Hypersonic Shock Tunnels
by: Khatta, Abhishek
Published: (2017)

An analytical investigation of the transient response time of a simulated supersonic wind tunnel pressure instrumentation system
by: Barnett, Lane
Published: (2006)

Supersonic refrigeration performances of nozzles and phase transition characteristics of wet natural gas considering shock wave effects
by: Xuewen Cao, et al.
Published: (2021-04-01)

Two-Dimensional Numerical Study of the Transient Flow ‎Conditions in Complete Shock Tunnel‎
by: A.M. Mohsen, et al.
Published: (2021-04-01)

Simulation of propagation and diffraction of a shock wave in a planar curvilinear channel
by: Pavel V. Bulat, et al.
Published: (2021-02-01)

Instability of transonic flow past flattened airfoils
by: Kuzmin Alexander
Published: (2013-12-01)

Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics
by: Bailey, Vincent Patrick, 1928-
Published: (1962)

Experimental Investigations on Supersonic Ejectors
by: Srisha Rao, M V
Published: (2018)

Influence of Mach Number of Main Flow on Film Cooling Characteristics under Supersonic Condition
by: Bo Zhang, et al.
Published: (2021-01-01)

Hypersonic and Supersonic Flight Advances in Aerodynamics, Materials, and Vehicle Design
Published: (2023)

Recent investigations of shock wave effects and interactions
by: P. M. Ligrani, et al.
Published: (2020-02-01)

Suppression of Low-Frequency Shock Oscillations over Boundary Layers by Repetitive Laser Pulse Energy Deposition
by: Akira Iwakawa, et al.
Published: (2016-04-01)

Numerical evaluation of shock wave effects on turbulent mixing layers in a scramjet combustor
by: Shizhuo Huang, et al.
Published: (2021-06-01)

Dynamic Stability of Heated Geometrically Irregular Shallow Shell of Constant Torsion in Supersonic Gas Flow
by: Belostochnyj, Grigorij Nikolaevich, et al.
Published: (2019-12-01)

Global Optimized Shapes of Flying Configurations Compared with Those of Gliding Birds
by: Adriana NASTASE
Published: (2014-04-01)

EFFECT OF BODY SHAPE ON THE AERODYNAMICS OF PROJECTILES AT SUPERSONIC SPEEDS
by: ABDULKAREEM SH. MAHDI, et al.
Published: (2008-12-01)

The production of hypersonic shock waves in an electrothermal diaphragm shock tube
by: Phillips, Malvern Gordon Rutherford
Published: (2011)

Approximate Analytical Models of Shock-Wave Structure at Steady Mach Reflection
by: Mikhail V. Chernyshov, et al.
Published: (2021-08-01)

APPLICABILITY OF VARIOUS DIFFERENTIAL TURBULENCE MODELS IN THE CALCULATION OF SUPERSONIC GAS JETS
by: E. E. Il'ina, et al.
Published: (2015-05-01)

Experimental And Theoretical Investigation Of Supersonic Flow Past Bodies With Elliptical Cross Section
by: Sharma, Rakesh Kumar
Published: (2012)

Hypersonic Vehicles Applications, Recent Advances, and Perspectives
Published: (2022)

WENO SCHEMES FOR SOLUTION OF UNSTEADY ONE-DIMENSIONAL GAS DYNAMICS TEST PROBLEMS
by: P. V. Bulat, et al.
Published: (2016-01-01)

An active control method for reducing sonic boom of supersonic aircraft
Published: (2021-06-01)

Numerical Simulation of Non-Equilibrium Two-Phase Wet Steam Flow through an Asymmetric Nozzle
by: Miah Md Ashraful Alam, et al.
Published: (2017-11-01)

Unique Design Discoveries for a Modern Mach 1.3 Airliner Including Anomalies in the Shock Wave Formation Along a Highly Swept Blunt Leading Edge Wing
Published: (2020)