Aerodynamics and Thermodynamics: Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration

Anatoly Michailovich Kharitonov; Mark Davidovich Brodetsky; Andreas Henze; Wolfgang Schröder; Matthias Heller; Gottfried Sachs; Christian Breitsamter; Boris Laschka

doi:10.1002/3527605711.ch4

Aerodynamics and Thermodynamics: Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration

Anatoly Michailovich Kharitonov, Mark Davidovich Brodetsky, Andreas Henze, Wolfgang Schröder, Matthias Heller, Gottfried Sachs, Christian Breitsamter, Boris Laschka

RWTH Aachen University

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

Abstract

Experimental and numerical findings for the supersonic flow field of the twostage vehicle ELAC/EOS are presented. The experiments have been performed in the T-313 wind tunnel of the Institute of Theoretical and Applied Mechanics, SB, Russian Academy of Sciences, in Novosibirsk. They include pressure, force, and moment measurements, and schlieren flow visualization. The numerical simulations provide the fully three dimensional data and are used to analyze the flow field by visualizing wall streamlines and the inner structure of the flow field. The first configuration of the investigation is the orbital stage EOS in close vicinity to a flat plate, while in the second part the separation of ELAC and EOS is modelled. The flow fields of these bodies strongly interfere and the influence of the interaction will be discussed in detail.

Original language	English
Title of host publication	Basic Research and Technologies for Two-Stage-to-Orbit Vehicles
Publisher	John Wiley and Sons
Pages	77-101
Number of pages	25
ISBN (Print)	3527277358, 9783527277353
DOIs	https://doi.org/10.1002/3527605711.ch4
State	Published - 7 Nov 2005

Keywords

Aerodynamics
Analysis of supersonic flow
Ascend and re-entry
ELAC-Model
ELAC-configuration
Flow physics
Flow simulation
Ground test facilities
High-enthalpy flows
Low-speed tests
Nonequilibrium air flows
Numerical simulation of high-enthalpy
Research
Technologies for two-stage-to-orbit vehicles
Thermodynamics
Two-stage ELAC/EOS-configuration

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10.1002/3527605711.ch4

Cite this

Kharitonov, A. M., Brodetsky, M. D., Henze, A., Schröder, W., Heller, M., Sachs, G., Breitsamter, C., & Laschka, B. (2005). Aerodynamics and Thermodynamics: Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration. In Basic Research and Technologies for Two-Stage-to-Orbit Vehicles (pp. 77-101). John Wiley and Sons. https://doi.org/10.1002/3527605711.ch4

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abstract = "Experimental and numerical findings for the supersonic flow field of the twostage vehicle ELAC/EOS are presented. The experiments have been performed in the T-313 wind tunnel of the Institute of Theoretical and Applied Mechanics, SB, Russian Academy of Sciences, in Novosibirsk. They include pressure, force, and moment measurements, and schlieren flow visualization. The numerical simulations provide the fully three dimensional data and are used to analyze the flow field by visualizing wall streamlines and the inner structure of the flow field. The first configuration of the investigation is the orbital stage EOS in close vicinity to a flat plate, while in the second part the separation of ELAC and EOS is modelled. The flow fields of these bodies strongly interfere and the influence of the interaction will be discussed in detail.",

keywords = "Aerodynamics, Analysis of supersonic flow, Ascend and re-entry, ELAC-Model, ELAC-configuration, Flow physics, Flow simulation, Ground test facilities, High-enthalpy flows, Low-speed tests, Nonequilibrium air flows, Numerical simulation of high-enthalpy, Research, Technologies for two-stage-to-orbit vehicles, Thermodynamics, Two-stage ELAC/EOS-configuration",

author = "Kharitonov, {Anatoly Michailovich} and Brodetsky, {Mark Davidovich} and Andreas Henze and Wolfgang Schr{\"o}der and Matthias Heller and Gottfried Sachs and Christian Breitsamter and Boris Laschka",

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month = nov,

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doi = "10.1002/3527605711.ch4",

language = "English",

isbn = "3527277358",

pages = "77--101",

booktitle = "Basic Research and Technologies for Two-Stage-to-Orbit Vehicles",

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Aerodynamics and Thermodynamics: Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration. / Kharitonov, Anatoly Michailovich; Brodetsky, Mark Davidovich; Henze, Andreas et al.
Basic Research and Technologies for Two-Stage-to-Orbit Vehicles. John Wiley and Sons, 2005. p. 77-101.

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

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T1 - Aerodynamics and Thermodynamics

T2 - Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration

AU - Kharitonov, Anatoly Michailovich

AU - Brodetsky, Mark Davidovich

AU - Henze, Andreas

AU - Schröder, Wolfgang

AU - Heller, Matthias

AU - Sachs, Gottfried

AU - Breitsamter, Christian

AU - Laschka, Boris

PY - 2005/11/7

Y1 - 2005/11/7

N2 - Experimental and numerical findings for the supersonic flow field of the twostage vehicle ELAC/EOS are presented. The experiments have been performed in the T-313 wind tunnel of the Institute of Theoretical and Applied Mechanics, SB, Russian Academy of Sciences, in Novosibirsk. They include pressure, force, and moment measurements, and schlieren flow visualization. The numerical simulations provide the fully three dimensional data and are used to analyze the flow field by visualizing wall streamlines and the inner structure of the flow field. The first configuration of the investigation is the orbital stage EOS in close vicinity to a flat plate, while in the second part the separation of ELAC and EOS is modelled. The flow fields of these bodies strongly interfere and the influence of the interaction will be discussed in detail.

AB - Experimental and numerical findings for the supersonic flow field of the twostage vehicle ELAC/EOS are presented. The experiments have been performed in the T-313 wind tunnel of the Institute of Theoretical and Applied Mechanics, SB, Russian Academy of Sciences, in Novosibirsk. They include pressure, force, and moment measurements, and schlieren flow visualization. The numerical simulations provide the fully three dimensional data and are used to analyze the flow field by visualizing wall streamlines and the inner structure of the flow field. The first configuration of the investigation is the orbital stage EOS in close vicinity to a flat plate, while in the second part the separation of ELAC and EOS is modelled. The flow fields of these bodies strongly interfere and the influence of the interaction will be discussed in detail.

KW - Aerodynamics

KW - Analysis of supersonic flow

KW - Ascend and re-entry

KW - ELAC-Model

KW - ELAC-configuration

KW - Flow physics

KW - Flow simulation

KW - Ground test facilities

KW - High-enthalpy flows

KW - Low-speed tests

KW - Nonequilibrium air flows

KW - Numerical simulation of high-enthalpy

KW - Research

KW - Technologies for two-stage-to-orbit vehicles

KW - Thermodynamics

KW - Two-stage ELAC/EOS-configuration

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DO - 10.1002/3527605711.ch4

M3 - Chapter

AN - SCOPUS:84891036061

SN - 3527277358

SN - 9783527277353

SP - 77

EP - 101

BT - Basic Research and Technologies for Two-Stage-to-Orbit Vehicles

PB - John Wiley and Sons

ER -

Aerodynamics and Thermodynamics: Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration

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Keywords

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