Add to ORKGThis paper deals with the usage of the TDLM in the Fairchild Dornier 728JET program, the first complete aircraft application of the TDLM. At first a description of the theory of the TDLM is given. Second the procedure applied to use TDLM results during MSC/NASTRAN flutter calculations is presented. The presentation closes with a comparison of DLM and TDLM based flutter calculations
Published in microfiche formSIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - ...
Flutter characteristics of a high T-Tail transport aircraft has been estimated using experimental mo...
Thesis: Ph. D., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2...
In this paper, a Transonic Doublet Lattice Method (TDLM) for calculating unsteady transonic pressure...
For assessment of the applicability of the Transonic Doublet Lattice Method (TDLM) to transonic flut...
In this report, a Transonic Doublet Lattice Method (TDLM) for calculating unsteady transonic pressur...
With increasing size and flexibility of new transport aircraft, aeroelastic effects become more and ...
Three different levels of unsteady CFD methods are used for transonic aeroelastic computations at DL...
Aerodynamic simulations were performed in order to compute the unsteady load response of the NLR 730...
In order to investigate aeroelastic aspects of engine/airframe integration, a simulation chain is se...
The Transonic Dynamics Tunnel (TDT) became in operational in 1960, and since that time has achieved ...
© 2019 by Max Opgenoord, Mark Drela, and Karen Willcox. Transonic aeroelasticity is an important con...
The process chain of the aeroelasic flutter analysis for new aircraft configurations is presented in...
A new ROM for a CFD based flutter analysis at transonic and separated flow conditions is presented. ...
Abstract. The development of a methodology for determining the flutter conditions of supercritical w...
Published in microfiche formSIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - ...
Flutter characteristics of a high T-Tail transport aircraft has been estimated using experimental mo...
Thesis: Ph. D., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2...
In this paper, a Transonic Doublet Lattice Method (TDLM) for calculating unsteady transonic pressure...
For assessment of the applicability of the Transonic Doublet Lattice Method (TDLM) to transonic flut...
In this report, a Transonic Doublet Lattice Method (TDLM) for calculating unsteady transonic pressur...
With increasing size and flexibility of new transport aircraft, aeroelastic effects become more and ...
Three different levels of unsteady CFD methods are used for transonic aeroelastic computations at DL...
Aerodynamic simulations were performed in order to compute the unsteady load response of the NLR 730...
In order to investigate aeroelastic aspects of engine/airframe integration, a simulation chain is se...
The Transonic Dynamics Tunnel (TDT) became in operational in 1960, and since that time has achieved ...
© 2019 by Max Opgenoord, Mark Drela, and Karen Willcox. Transonic aeroelasticity is an important con...
The process chain of the aeroelasic flutter analysis for new aircraft configurations is presented in...
A new ROM for a CFD based flutter analysis at transonic and separated flow conditions is presented. ...
Abstract. The development of a methodology for determining the flutter conditions of supercritical w...
Published in microfiche formSIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - ...
Flutter characteristics of a high T-Tail transport aircraft has been estimated using experimental mo...
Thesis: Ph. D., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2...