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Flugmechanik
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The NASA High Speed ASE Project: Computational Analyses of a Low-Boom Supersonic Configuration
Status of the KTH-NASA Wind-Tunnel Test for Acquisition of Transonic Nonlinear Aeroelastic Data
Reduced-Order Models for the Aeroelastic Analysis of Ares Launch Vehicles
Pressure measurements on a rectangular wing with a NACA0012 airfoil during conventional flutter
Investigation of the aeroelastic stability of the AFW wind-tunnel model using CAP-TSD
Investigation of the aeroelastic stability of the AFW wind-tunnel model using CAP-TSD
Improving CAP-TSD steady pressure solutions through airfoil slope modification
Experimental transonic flutter characteristics of two 72 deg-sweep delta-wing models
Computational Aeroelastic Analysis of the Semi-Span Super-Sonic Transport (S4T) Wind-Tunnel Model
Computational Aeroelastic Analyses of a Low-Boom Supersonic Configuration
A Status Review of the Commercial Supersonic Technology (CST) Aeroservoelasticity (ASE) Project
Application of nonlinear systems theory to transonic unsteady aerodynamic responses
Aeroelastic Response of Swept Aircraft Wings in a Compressible Flow Field
Aeroelastic Indicial Response Reduced-Order Modeling for Flexible Flight Vehicles
Aeroelastic Indicial Response Reduced-Order Modeling for Flexible Flight Vehicles