Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Arsenio Dimanlig"'
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
In this paper, we present the validation of the multi-disciplinary rotorcraft simulation code Helios for its ability to predict the blade-vortex interactions(BVI) and the rotor wake in the descending flight. Helios uses a dual-mesh paradigm with unst
Publikováno v:
2010 DoD High Performance Computing Modernization Program Users Group Conference.
To address the complex multidisciplinary nature of rotorcraft analysis, high-fidelity computational fluid and structural dynamics models have been developed to investigate a range of challenging rotorcraft issues. First, an advanced technology, activ
Publikováno v:
2009 DoD High Performance Computing Modernization Program Users Group Conference.
To address the complex multidisciplinary nature of rotorcraft analysis, high-fidelity computational fluid and structural dynamics models have been developed for an advanced technology, active flap rotor. Comparisons are made between computational flu
Publikováno v:
2008 DoD HPCMP Users Group Conference.
This paper presents work done on modeling the CH-47 tandem rotor helicopter with fuselage in high speed forward flight using computational fluid dynamics coupled with a comprehensive rotorcraft analysis tool. The flow calculations and subsequent airl
Autor:
Roger C. Strawn, Mark Potsdam, Tor Anders Nygaard, Hossein Saberi, Arsenio Dimanlig, Robert A. Ormiston, Mahendra J. Bhagwat
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference and Exhibit.
Publikováno v:
2007 DoD High Performance Computing Modernization Program Users Group Conference.
This paper describes installed rotor performance computations for the CH-47 Chinook tandem-rotor helicopter. The computations were performed with a Reynolds-Averaged Navier-Stokes flow solver using overset structured grids to resolve the flow around
Publikováno v:
Annals of the New York Academy of Sciences. 974
The cell culture unit (CCU) is being designed to support cell growth for long-duration life science experiments on the International Space Station (ISS). The CCU is a perfused loop system that provides a fluid environment for controlled cell growth e
Publikováno v:
Annals of the New York Academy of Sciences; 2002, Vol. 974 Issue 1, p518-540, 23p