Simulation validation of static and forced motion flow physics of a canard configured TransCruiser

Author:

Ghoreyshi Mehdi,Korkis-Kanaan Ramy,Jirásek Adam,Cummings Russell M.,Lofthouse Andrew J.

Funder

USAFA

High Performance Computing Research Center at USAFA

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. Design of a canard configured TransCruiser using CEASIOM;Rizzi;Prog. Aerosp. Sci.,2011

2. Reynolds-averaged Navier–Stokes technology for transonic drag prediction: a boeing perspective;Mani;J. Aircr.,2014

3. Virtual-aircraft design & control of TransCruiser – a canard configuration;Rizzi,2010

4. R. Von Kaenel, A. Rizzi, J. Oppelstrup, T. Grabowski, M. Ghoreyshi, L. Cavagna, A. Bérard, CEASIOM: simulating stability & control with CFD/CSM in aircraft conceptual design, in: 26th International Congress of the Aeronautical Sciences, ICAS, 14–19 September 2008, Anchorage, Alaska, USA.

5. Virtual aircraft design of TransCruiser – computing break points in pitch moment curve;Eliasson,2010

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