H. Koester

Numerical Investigation on Two Airfoil Design Codes Based on the Euler and Navier-Stokes Equations (1995)

Hua, J., Redeker, G., Koester, H., Bartelheimer, W.

Under the framework of the DLR-CAE cooperation topic: 92-16, numerical investigation is carried out on two airfoil analysis/ design codes at the Institute of Design Aerodynamics, DLR, Braunschweig....

Numerical Investigation on Two Airfoil Analysis Codes Using the Euler and Navier-Stokes Equations in Inviscid and Viscous Flows (1995)

Hua, J., Redeker, G., Koester, H., Bartelheimer, W.

Under the framework of the DLR-CAE cooperation topic: 92-16, numerical investigation is carried out on two transonic airfoil analysis/design codes at the Institute of Design Aerodynamics, DLR,...

a) The Transonic Wind Tunnel Braunschweig b) The determination of Limiting N-Factors of TWB c) Design of a Natural Laminar Flow Airfoil for a Commuter Aircraft d) Design of a Natural Laminar Flow Glove for a Transport Aircraft e) Investigations of Airfoil DLR-LV2 in the Cryogenic Wind Tunnel T2 of ONERA (1994)

H. Koester

Trailing Edge Optimization Investigations on A320-Wing (1994)

Koester, H., Wichmann, G.

This report contains the results of pressure and friction drag calculations of the A320 wing and its TEO modification. It could be shown that the modified TEO wing provides some advantages compared...

Numerical Design Method for Modern NLF FAirfoils (1993)

Hua, Jun (1), Zhang Zhong-yin (2), Shi Ninguang (3), Redeker, G., Koester, H.

Investigations of Airfoils with Cambered Trailing Edges (1993)

Koester, H.

Neue Entwicklungen in der Hubschrauberaerodynamik Teil I: Profile fuer Hubschrauber. (1993)

Koester, H.

Airfoil Investigations with Modified Trailing Edge II. (1992)

Koester, H.

Investigation and Improvement of Two Design Codes for Transonic Airfoils. (1992)

Hua, J., Koester, H.

Ueber die Originalität des Byronschen Manfred, eine philologische Untersuchung (1842)

Koester, H.

25 p.