Benutzer: Gast  Login
Titel:

EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A STRUCTURAL-DYNAMICALLY SCALED DELTA WING WITH TRAILING EDGE FLAPS

Dokumenttyp:
Konferenzbeitrag
Art des Konferenzbeitrags:
Textbeitrag / Aufsatz
Autor(en):
Bantscheff, Konstantin; Santelli, Francesco; Breitsamter, Christian
Abstract:
This work focuses on an experimental investigations of a delta wing fuselage configuration in the low-speed wind tunnel W/T-A facility of the Chair of Aerodynamics and Fluid Mechanics at the Technical University of Munich. The influence of different trailing edge flap deflections on the aerodynamic characteristics is studied. For the aerodynamic analyses, force and moment measurements, Particle Image Velocimetry (PIV) measurements and a Fast Response Aerodynamic Probe (FRAP) measurement are cond...     »
Stichworte:
Aeroelasticity; Delta wing; Fast Response Aerodynamic Probe
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
34th Congress of the International Council of the Aeronautical Sciences, ICAS 2024
Datum der Konferenz:
9 September 2024through 13 September 2024
Verlag / Institution:
International Council of the Aeronautical Sciences
Jahr:
2024
Nachgewiesen in:
Scopus
Serien-ISSN:
10259090
Sprache:
en
WWW:
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85208791079&partnerID=40&md5=699e64356e79d069df728e6a594aaf07
TUM Einrichtung:
Lehrstuhl für Aerodynamik und Strömungsmechanik
 BibTeX