On May 5th 2023, the administration board of HyFAR-ARA officially validated CNES as new member of the association.
The French space agency (CNES, Centre National d'Etudes Spatiales) is a public administration with industrial and commercial…
Adjoint-based linear sensitivity of a hypersonic boundary layer to steady wall blowing or heating
Arthur POULAIN¹, Denis SIPP¹*, Cédric CONTENT¹, Georgios RIGAS², Eric GARNIER¹
¹ DAAA, ONERA, Université Paris Saclay, F-92190 Meudon,…
https://www.hyfar-ara.org/wp-content/uploads/2023/06/02-Sipp-842x600px-300ppp.png600842dominique pirotaishttps://www.hyfar-ara.org/wp-content/uploads/2020/02/unnamed.pngdominique pirotais2023-06-20 13:01:012023-06-20 13:02:512-WALL BLOWING AND HEATING
Fundamental breakdown of second modes in the High Enthalpy Shock Tunnel Göttingen
Divek SURUJHLAL 1 *, Alexander WAGNER 2
* Corresponding author
1German Aerospace Center (DLR) Göttingen, Department of Spacecraft surujhlal@dlr.de…
https://www.hyfar-ara.org/wp-content/uploads/2023/06/image-blog.jpg500755dominique pirotaishttps://www.hyfar-ara.org/wp-content/uploads/2020/02/unnamed.pngdominique pirotais2023-06-20 12:43:432023-06-20 13:02:343-breakdown of second modes
Experimental investigation of the transition process and boundary layer separation on a hypersonic cone-cylinder-flare geometry
Clément Caillaud 2, Mathieu Lugrin ∗,1, Sébastien Esquieu 2
1DAAA, ONERA, Paris Saclay University, F-92190…
OCTRA as Ultrasonically Absorptive Thermal Protection Material for Hypersonic Transition Suppression analyzed on a 7° Cone
Viola WARTEMANN 1*, Alexander WAGNER2, Divek SURUJHLAL3, Giannino PONCHIO CAMILLO4, Christian DITTERT 5, Carolin…
https://www.hyfar-ara.org/wp-content/uploads/2023/06/06-Wartemann-fig1-cone-with-porous-material-850x500px.jpg500850dominique pirotaishttps://www.hyfar-ara.org/wp-content/uploads/2020/02/unnamed.pngdominique pirotais2023-06-17 15:23:372023-06-17 15:45:416-Ultrasonically Absorptive material
Numerical investigation of the transition process and boundary layer separation on a hypersonic cone-cylinder-flare geometry
Clément Caillaud*,1, Mathieu Lugrin 2, Sébastien Esquieu 1
1CEA-CESTA, 15 Avenue des Sablières, Le Barp, France
2DAAA,…
A New Approach towards Tailored Thermal Protection Material for Hypersonic Boundary Layer Control
Alexander Wagner1(*), Divek Surujhlal1, Carolin Rauh2, Martin Frieß2, Fiona Kessel2, Hendrik Weihs2
1Institute of Aerodynamic…
Laminar-Turbulent Transition on the STORT Flight Experiment
Sebastian Willems *1, Florian Klingenberg.#1, Frank Sieb ◊1, Ali Gülhan §1,
Thomas Reimer ‡2, Giuseppe Di Martino.†2, Dorian Hargarten **3,
and Maximilian Zurkaulen.ƚ3
1Supersonic…
https://www.hyfar-ara.org/wp-content/uploads/2023/06/09-Willems-b.jpg710553dominique pirotaishttps://www.hyfar-ara.org/wp-content/uploads/2020/02/unnamed.pngdominique pirotais2023-06-15 19:57:452023-06-15 20:15:409-Stort flight test
Experimental investigation of boundary layer instabilities and transition on sharp and blunt cones in Oxford’s High-Density Tunnel
Andrew P. Ceruzzi , andrew.ceruzzi@eng.ox.ac.uk
corresponding author,
Laurent M. Le Page, laurent.lepage@eng.ox.ac.uk
Philipp…
THE CNES JOINS HyFAR-ARA
News1-vehicle design criteria
TRANSITION 20232-WALL BLOWING AND HEATING
TRANSITION 20233-breakdown of second modes
TRANSITION 20235-cone-cylinder-flare experiment
TRANSITION 20236-Ultrasonically Absorptive material
TRANSITION 20237-Cone-cylinder flare analysis
TRANSITION 20238-Ultrasonic absorptive TPS
TRANSITION 20239-Stort flight test
TRANSITION 202310-Boundary layer experiments
TRANSITION 2023