Flow characterization of the Mach 5 hypersonic nozzle of VKI-H3 wind tunnel
Gyenge, Akos ; Cakir, Bora O. LU
; Grossir, Guillaume
; Saracoglu, Bayindir H.
and Chazot, Olivier
(2024)
AIAA SciTech Forum and Exposition, 2024
In AIAA SciTech Forum and Exposition, 2024
- Abstract
The operational map of the H3 Mach 6 blowdown wind tunnel, at the von Karman Institute for Fluid Dynamics (VKI), is extended towards lower Mach numbers with a new axisymmetric contoured nozzle to achieve Mach 5 testing conditions. Following the design, manufacturing, instrumentation and integration of the Mach 5 nozzle, an extensive commissioning campaign is initiated. The flow investigations rely on several intrusive and non-intrusive measurement techniques including free-stream static pressure measurements, a rake of pitot probes, total temperature probes and schlieren flow visualization. Results are compared with numerical predictions.
Please use this url to cite or link to this publication:
https://lup.lub.lu.se/record/81f519be-c209-40cd-b113-48d40cc863af
- author
- Gyenge, Akos
; Cakir, Bora O.
LU
; Grossir, Guillaume
; Saracoglu, Bayindir H.
and Chazot, Olivier
- organization
- publishing date
- 2024
- type
- Chapter in Book/Report/Conference proceeding
- publication status
- published
- subject
- host publication
- AIAA SciTech Forum and Exposition, 2024
- series title
- AIAA SciTech Forum and Exposition, 2024
- publisher
- American Institute of Aeronautics and Astronautics
- conference name
- AIAA SciTech Forum and Exposition, 2024
- conference location
- Orlando, United States
- conference dates
- 2024-01-08 - 2024-01-12
- external identifiers
-
- scopus:85196830519
- ISBN
- 9781624107115
- DOI
- 10.2514/6.2024-2210
- language
- English
- LU publication?
- yes
- id
- 81f519be-c209-40cd-b113-48d40cc863af
- date added to LUP
- 2024-09-04 15:18:06
- date last changed
- 2025-04-04 14:55:48
@inproceedings{81f519be-c209-40cd-b113-48d40cc863af,
abstract = {{<p>The operational map of the H3 Mach 6 blowdown wind tunnel, at the von Karman Institute for Fluid Dynamics (VKI), is extended towards lower Mach numbers with a new axisymmetric contoured nozzle to achieve Mach 5 testing conditions. Following the design, manufacturing, instrumentation and integration of the Mach 5 nozzle, an extensive commissioning campaign is initiated. The flow investigations rely on several intrusive and non-intrusive measurement techniques including free-stream static pressure measurements, a rake of pitot probes, total temperature probes and schlieren flow visualization. Results are compared with numerical predictions.</p>}},
author = {{Gyenge, Akos and Cakir, Bora O. and Grossir, Guillaume and Saracoglu, Bayindir H. and Chazot, Olivier}},
booktitle = {{AIAA SciTech Forum and Exposition, 2024}},
isbn = {{9781624107115}},
language = {{eng}},
publisher = {{American Institute of Aeronautics and Astronautics}},
series = {{AIAA SciTech Forum and Exposition, 2024}},
title = {{Flow characterization of the Mach 5 hypersonic nozzle of VKI-H3 wind tunnel}},
url = {{http://dx.doi.org/10.2514/6.2024-2210}},
doi = {{10.2514/6.2024-2210}},
year = {{2024}},
}