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Evaluation of Future Aerodynamic Technologies for High Capacity Aircraft

Strohmeyer, D. and Seubert, R. and Heinze, W. and Österheld, C. and Fornasier, L. (1999) Evaluation of Future Aerodynamic Technologies for High Capacity Aircraft. 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno (ne), 11.-14.01.1999.

Full text not available from this repository.

Abstract

For the analysis of a three surface Megaliner configuration a preliminary aircraft design code was extended by a higher-order panel method, a transonic data base and a trim routine. Preliminary results of the design studies show that the integration of the canard as lifting control device promises a significant reduction of the drag (3A%) and mission fuel (2.3%).

Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Evaluation of Future Aerodynamic Technologies for High Capacity Aircraft
Authors:
AuthorsInstitution or Email of Authors
Strohmeyer, D.UNSPECIFIED
Seubert, R.UNSPECIFIED
Heinze, W.UNSPECIFIED
Österheld, C.UNSPECIFIED
Fornasier, L.UNSPECIFIED
Date:1999
Status:Published
Keywords:Preliminary Aircraft Design, PRADO, Panel code, HISSS, Megaliner, Three Surface Aircraft, Canard Design
Event Title:37th AIAA Aerospace Sciences Meeting and Exhibit, Reno (ne), 11.-14.01.1999
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Concepts & Integration
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: Claudia Grant
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:06

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