Zobrazeno 1 - 10
of 10
pro vyhledávání: '"David Rohlmann"'
Publikováno v:
2018 Atmospheric and Space Environments Conference.
Publikováno v:
2018 Atmospheric and Space Environments Conference.
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783319211268
The objective of the joint research project HINVA (High-Lift In-Flight Validation) funded by the German Federal Ministry of Economics and Technology within the fourth Aeronautical Research Program LuFo IV is to significantly enhance the accuracy and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bfcdbfd60d894b4e1c3cde4465a568cd
https://doi.org/10.1007/978-3-319-21127-5_20
https://doi.org/10.1007/978-3-319-21127-5_20
Autor:
Stefan Keye, David Rohlmann
Publikováno v:
33rd AIAA Applied Aerodynamics Conference.
Within the German national research project HINVA (High-lift INflight VAlidation) the prediction of maximum lift of realistic transport aircraft configurations should be improved. To understand also the dynamic aerodynamic and aeroelastic effects of
Autor:
David Rohlmann
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783319211268
Within the German national research project HINVA (High-lift INflight VAlidation) the prediction of maximum lift of realistic transport aircraft configurations shall be improved. This is achieved by a close link of flight tests, cryogenic wind tunnel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ebb73f8c28fd7fffdc9f658101ef5cb7
https://elib.dlr.de/99944/
https://elib.dlr.de/99944/
Aeroelastic Effects in Maximum Lift Prediction of a Transport Aircraft and Comparison to Flight Data
Autor:
Stefan Keye, David Rohlmann
The virtual determination of maximum lift performance of a transport aircraft configuration taking into account static aeroelastic deformations at steady-state flight conditions is described. Within the scope of the national research project HINVA (H
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f4beb91198232775636a9feb82ae004c
https://elib.dlr.de/97707/
https://elib.dlr.de/97707/
Publikováno v:
31st AIAA Applied Aerodynamics Conference.
The objective of the joint research project HINVA (High-Lift In-Flight Validation) funded by the German Federal Ministry of Economics and Technology within the fourth Aeronautical Research Program LuFo IV is to significantly enhance the accuracy and
The present study aims at assessing the influence of the interference effects caused by the horizontal tail plane (HTP) and vertical tail plane (VTP) on the aerodynamic behaviour of a transport aircraft in high-lift configuration. This aspect is of p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7a8e433faa48b0db95ebc4d54416f533
https://elib.dlr.de/78217/
https://elib.dlr.de/78217/
Within task three “Numerical Simulations” in the project “HINVA - High Lift INflight Validation” extensive numerical verification studies based on a CAD model of DLR’s A320232 "Advanced Technology Research Aircraft" in landing configuration
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6d461ff6f3c8849d4723e858979f95b0
https://elib.dlr.de/74446/
https://elib.dlr.de/74446/
Publikováno v:
Scopus-Elsevier
The final approach and touchdown of a landing aircraft is studied numerically with different hybrid Reynolds-averaged Navier–Stokes (RANS)/large-eddy simulations (LES) approaches. Particular emphas...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2209d63aeab217b2482e2196d761a93e
http://www.scopus.com/inward/record.url?eid=2-s2.0-85077278160&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-85077278160&partnerID=MN8TOARS