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:

Authors	Institution or Email of Authors
Strohmeyer, D.
Seubert, R.
Heinze, W.
Österheld, C.
Fornasier, L.

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

HGF - Program:

Aeronautics

HGF - Program Themes:

L - no assignement

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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