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Morphing of Flying Configuration Using Spanwise Movable Leading Edge Flaps, in Supersonic Flow
Author(s) -
Nastase Adriana
Publication year - 2011
Publication title -
pamm
Language(s) - English
Resource type - Journals
ISSN - 1617-7061
DOI - 10.1002/pamm.201110279
Subject(s) - fuselage , morphing , leading edge , wing , computation , enhanced data rates for gsm evolution , flow (mathematics) , supersonic speed , position (finance) , aerospace engineering , mechanics , computer science , structural engineering , engineering , physics , telecommunications , artificial intelligence , algorithm , finance , economics
The computation of the flow over flattened wing‐fuselage flying configuration (FC) with movable leading edge flaps in spanwise direction is here considered. Hyperbolical potential solutions are given in closed form and are used for the determination of hybrid solutions for the Navier‐Stokes layer, over this FC with the flaps in retracted and in open position. (© 2011 Wiley‐VCH Verlag GmbH & Co. KGaA, Weinheim)