Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Heiko von Geyr"'
Autor:
Geza Schrauf, Heiko von Geyr
Publikováno v:
Journal of Aircraft. 58:1272-1280
A flight test with a simplified hybrid laminar flow control (HLFC) system on the vertical tail plane (VTP) of an A320 aircraft was performed in April/May 2018. This HLFC system was a prototype for ...
Autor:
Heiko von Geyr, Geza H. Schrauf
A flight test with a simplified HLFC system on the vertical tail plane of an A320 aircraft was performed in April/May 2018. In this paper we discuss the preparation of the flight test data for evaluation with linear stability theory on the basis of s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2c84f7877de5a472b836ab4a265938d3
https://elib.dlr.de/140677/
https://elib.dlr.de/140677/
Autor:
Heiko von Geyr, Geza H. Schrauf
Publikováno v:
AIAA Scitech 2020 Forum.
A flight test with a simplified HLFC system on the vertical tail plane of an A320 aircraft was performed in April/May 2018. The aerodynamic and system design is discussed and first results of the flight tests are presented.
Publikováno v:
Aerospace Science and Technology. 6:31-42
Due to a trend towards very high-bypass ratio engines and a corresponding close coupling of engine and airframe, the minimization of adverse interference effects is an important aspect in aircraft design. Investigations of engine/airframe integration
Autor:
Ralf Rudnik, Heiko von Geyr
Publikováno v:
25th AIAA Applied Aerodynamics Conference.
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
The development and application of a MDO process for the design of range maximised high-speed transport aircraft is described. The complete flight mission from take-off to landing is modelled. For supersonic cruise conditions the disciplines aerodyna