Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Inna Kurits"'
Publikováno v:
AIAA Scitech 2021 Forum.
Publikováno v:
AIAA Scitech 2020 Forum.
Publikováno v:
AIAA Scitech 2019 Forum.
Autor:
Mark J. Lewis, Inna Kurits
Publikováno v:
Journal of Thermophysics and Heat Transfer. 23:256-266
A quantitative global intensity-based temperature-sensitive paint heat transfer measurement system has been developed at Arnold Engineering Development Center Hypervelocity Wind Tunnel No. 9. The system has been designed for use with metal wind-tunne
Autor:
Joseph J. Coblish, John Lafferty, Joseph D. Norris, Michael Marana, Eric C. Marineau, Michael W. Smith, Inna Kurits, Daniel R. Lewis
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Hypervelocity Wind Tunnel No. 9, located at the White Oak, MD site of the Arnold Engineering Development Complex (AEDC), has long been recognized as a unique world class ground-test facility. The facility was developed in the early 1970s to provide c
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Aerodynamic heating is a critical parameter in hypersonic vehicle design. Ground-test facilities employ a variety of discrete sensors and global techniques to characterize the heating on the surfaces of a test article. AEDC Hypervelocity Wind Tunnel
Autor:
Inna Kurits, Joseph D. Norris
Publikováno v:
27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
The AEDC Hypervelocity Wind Tunnel No. 9 is a ground-test facility that features a unique combination of flow conditions, run times, and physical size not reproduced anywhere else in the world. By taking advantage of its large size and long run times
Publikováno v:
26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
A quantitative global intensity-based temperature-sensitive paint heat-transfer measurement system has been developed for use in AEDC Hypervelocity Wind Tunnel No. 9. A numerical data reduction approach has been proposed for calculating the convectiv
Publikováno v:
2007 22nd International Congress on Instrumentation in Aerospace Simulation Facilities.
Heat-transfer rates are an extremely important consideration in the design of hypersonic vehicles such as atmospheric reentry vehicles. This paper describes the development of a data reduction methodology to evaluate heat-transfer rates using global