Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Joseph D. Norris"'
Autor:
Brian R. Hollis, Joseph J. Coblish, Thomas J. Horvath, Benjamin S. Kirk, Karen T. Berger, Joseph D. Norris, Randolph P. Lillard
Publikováno v:
Journal of Spacecraft and Rockets. 46:766-780
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
Autor:
Joseph D. Norris, John Lafferty, Heath B. Johnson, Daniel R. Lewis, Eric C. Marineau, C. George Moraru
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
The boundary-layer transition and stability characteristics of sharp cones at angle-of-attack are investigated with measurements at Mach 10 in the Arnold Engineering Development Complex (AEDC) Hypervelocity Wind Tunnel 9 on a 1.5-m long, 7-deg cone a
Autor:
John Lafferty, George C. Moraru, Eric C. Marineau, Daniel R. Lewis, Justin Smith, Ross Wagnild, Joseph D. Norris
Publikováno v:
19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Boundary-layer transition and stability data were obtained at Mach 10 in the Arnold Engineering Development Complex (AEDC) Hypervelocity Wind Tunnel 9 on a 1.5-m long, 7-deg cone at unit Reynolds numbers between 1.8 and 31 million per meter. A total
Autor:
Ndaona Chokani, Joseph D. Norris
Publikováno v:
AIAA Journal. 41:1619-1621
References 1“Assessment ofExperimentalUncertaintywithApplicationtoWindTunnel Testing,” AIAA Standard S-071A-1999, Revision A of the Standard, AIAA, Reston, VA, 1999, pp. 11–17. 2Coleman, H. W., and Steele, W. G., Experimentation and Uncertainty
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
Autor:
Joseph D. Norris, Daniel R. Lewis
Publikováno v:
26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
Arnold Engineering Development Center (AEDC) Tunnel 9 has recently developed a technique to measure transient heat-transfer rates on roughened model surfaces using the thin-skin measurement technique. The thin-skin technique is used to obtain the hea
Autor:
Benjamin S. Kirk, Thomas J. Horvath, Joseph J. Coblish, Brian R. Hollis, Randolph P. Lillard, Joseph D. Norris, Karen T. Berger
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
An investigation of the aeroheating environment of the Project Orion Crew Exploration Vehicle was performed in the Arnold Engineering Development Center Hypervelocity Wind Tunnel No. 9 Mach 8 and Mach 10 nozzles and in the NASA Langley Research Cente
Autor:
Joseph D. Norris, John Lafferty
Publikováno v:
2007 U.S. Air Force T&E Days.
The Arnold Engineering Development Center (AEDC) Hypervelocity Wind Tunnel No. 9 facility has played a key role in the development of hypersonic vehicles for over 30 years, providing high-quality aerodynamic and aerothermal test data covering high Ma