Zobrazeno 1 - 10
of 23
pro vyhledávání: '"Nicholas F. Giannelis"'
Publikováno v:
Aerospace, Vol 10, Iss 9, p 746 (2023)
This paper introduces a generic model for the study of aerodynamic behaviour relevant to fifth-generation high-performance aircraft. The model design is presented, outlining simplifications made to retain the key features of modern high-performance v
Externí odkaz:
https://doaj.org/article/8add2cf1ec6f4334b972047f4ca2282a
Publikováno v:
Fluids, Vol 5, Iss 2, p 46 (2020)
At transonic flight conditions, shock oscillations on wing surfaces are known to occur and result in degraded aerodynamic performance and handling qualities. This is a purely flow-driven phenomenon, known as transonic buffet, that causes limit cycle
Externí odkaz:
https://doaj.org/article/b03e281cc6364d70b9f49723f483b791
Publikováno v:
AIAA SCITECH 2023 Forum.
Autor:
Nicholas F. Giannelis, Gareth A. Vio
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2022 Forum.
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
Nicholas F. Giannelis, Gareth A. Vio
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
Caroline O. Hamilton Smith, Ben Thornber, Gareth A. Vio, Adam J. Murray, Nicholas F. Giannelis
Publikováno v:
AIAA Scitech 2021 Forum.
Publikováno v:
Fluids
Volume 5
Issue 2
Fluids, Vol 5, Iss 46, p 46 (2020)
Volume 5
Issue 2
Fluids, Vol 5, Iss 46, p 46 (2020)
At transonic flight conditions, shock oscillations on wing surfaces are known to occur and result in degraded aerodynamic performance and handling qualities. This is a purely flow-driven phenomenon, known as transonic buffet, that causes limit cycle