Flow control effectiveness at high speed flows

K. Kontis; C. Lada

Flow control effectiveness at high speed flows

K. Kontis
, C. Lada

Research output: Chapter in Book/Conference proceeding › Conference contribution

Abstract

The effects of two important flow control techniques, i.e. jet control and dimples, on the aerodynamic characteristics and performance of a number of body configurations have been studied experimentally. The dimple studies have been carried out in a transonic-supersonic wind tunnel and the jet studies in a hypersonic gun tunnel at a Mach number of 8.2. Air was used as the working gas. The tests employed schlieren photography and oil-flow to study the overall flow field. Quantitative studies have been made by pressure measurements.

Original language	English
Title of host publication	European Space Agency, (Special Publication) ESA SP\|Eur Space Agency Spec Publ ESA SP
Editors	D. Danesy
Pages	609-614
Number of pages	5
Publication status	Published - 2004
Event	5th European Symposium on Aerothermodynamics for Space Vehicles - Cologne Duration: 1 Jul 2004 → …

Conference

Conference	5th European Symposium on Aerothermodynamics for Space Vehicles
City	Cologne
Period	1/07/04 → …

Cite this

@inproceedings{2fe8a29308d24bf89cdd8a9ddfdf8ac4,

title = "Flow control effectiveness at high speed flows",

abstract = "The effects of two important flow control techniques, i.e. jet control and dimples, on the aerodynamic characteristics and performance of a number of body configurations have been studied experimentally. The dimple studies have been carried out in a transonic-supersonic wind tunnel and the jet studies in a hypersonic gun tunnel at a Mach number of 8.2. Air was used as the working gas. The tests employed schlieren photography and oil-flow to study the overall flow field. Quantitative studies have been made by pressure measurements.",

author = "K. Kontis and C. Lada",

year = "2004",

language = "English",

pages = "609--614",

editor = "D. Danesy",

booktitle = "European Space Agency, (Special Publication) ESA SP|Eur Space Agency Spec Publ ESA SP",

note = "5th European Symposium on Aerothermodynamics for Space Vehicles ; Conference date: 01-07-2004",

}

TY - GEN

T1 - Flow control effectiveness at high speed flows

AU - Kontis, K.

AU - Lada, C.

PY - 2004

Y1 - 2004

N2 - The effects of two important flow control techniques, i.e. jet control and dimples, on the aerodynamic characteristics and performance of a number of body configurations have been studied experimentally. The dimple studies have been carried out in a transonic-supersonic wind tunnel and the jet studies in a hypersonic gun tunnel at a Mach number of 8.2. Air was used as the working gas. The tests employed schlieren photography and oil-flow to study the overall flow field. Quantitative studies have been made by pressure measurements.

AB - The effects of two important flow control techniques, i.e. jet control and dimples, on the aerodynamic characteristics and performance of a number of body configurations have been studied experimentally. The dimple studies have been carried out in a transonic-supersonic wind tunnel and the jet studies in a hypersonic gun tunnel at a Mach number of 8.2. Air was used as the working gas. The tests employed schlieren photography and oil-flow to study the overall flow field. Quantitative studies have been made by pressure measurements.

M3 - Conference contribution

SP - 609

EP - 614

BT - European Space Agency, (Special Publication) ESA SP|Eur Space Agency Spec Publ ESA SP

A2 - Danesy, D.

T2 - 5th European Symposium on Aerothermodynamics for Space Vehicles

Y2 - 1 July 2004

ER -

Flow control effectiveness at high speed flows

Abstract

Conference

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