Zobrazeno 1 - 10
of 23
pro vyhledávání: '"Shann J. Rufer"'
Autor:
Shann J. Rufer, Michael A. Kegerise
Publikováno v:
Exp Fluids
In this paper, we report on the application of the atomic layer thermopile (ALTP) heat-flux sensor to the measurement of laminar-to-turbulent transition in a hypersonic flat-plate boundary layer. The centerline of the flat-plate model was instrumente
Autor:
Tait Pottebaum, Charles H. Campbell, Vanessa V. Aubuchon, Shann J. Rufer, Richard J. Schwartz, Thomas S. Spisz, David Gibson, C. David Mercer, Steve Kennerly, Martin N. Ross, Thomas J. Horvath, Steven Tack, Kwame Osei-Wusu, Gordon Scriven
Publikováno v:
AIAA SPACE and Astronautics Forum and Exposition.
Autor:
Michelle L. Mason, Shann J. Rufer
Publikováno v:
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
The Imaging for Hypersonic Experimental Aeroheating Testing (IHEAT) software is used at the NASA Langley Research Center to analyze global aeroheating data on wind tunnel models tested in the Langley Aerothermodynamics Laboratory. One-dimensional, se
Autor:
Shann J. Rufer, Michael A. Kergerise
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
In this paper we report on the application of the atomic layer thermopile (ALTP) heat- flux sensor to the measurement of laminar-to-turbulent transition in a hypersonic flat plate boundary layer. The centerline of the flat-plate model was instrumente
Autor:
Brian R. Hollis, Karen T. Berger, Gregory M. Buck, Gregory J. Brauckmann, William A. Wood, Matthew N. Rhode, Thomas J. Horvath, Shann J. Rufer, Scott A. Berry, Derek S. Liechty, Kelly J. Murphy, Michelle L. Mason
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
A description of the NASA Langley Research Center’s Langley Aerothermodynamics Laboratory (LAL) will be presented in the paper, along with descriptions and details of the facility test techniques and recent upgrades. The LAL consists of three hyper
Autor:
Brian R. Hollis, Thomas J. Horvath, Michael DiFulvio, Mark Schoenenberger, Greg J. Brauckmann, Karen T. Berger, Shann J. Rufer, Gregory M. Buck, Derek S. Liechty, Scott A. Berry, N. R. Merski, Kelly J. Murphy
Publikováno v:
52nd Aerospace Sciences Meeting.
A review is presented of recent research, development, testing and evaluation activities related to entry, descent and landing that have been conducted at the NASA Langley Research Center. An overview of the test facilities, model development and fab
Autor:
Shann J. Rufer, Dennis C. Berridge
Publikováno v:
42nd AIAA Fluid Dynamics Conference and Exhibit.
Experiments have been carried out in the NASA Langley Research Center 20-Inch Mach 6 Wind Tunnel to measure the freestream pressure fluctuations, or tunnel noise, using a pitot rake. These experiments are part of an on-going effort to characterize th
Autor:
Shann J. Rufer, Dennis C. Berridge
Publikováno v:
41st AIAA Fluid Dynamics Conference and Exhibit.
Experiments have been carried out in the NASA Langley Research Center 20-Inch Mach 6 Air Tunnel to measure the second-mode boundary-layer instability on a 7° half-angle cone using high-frequency pressure sensors. Data were obtained with both blunt a
Autor:
Michael Holden, Brian Anderson, Matthew MacLean, Scott A. Berry, Charles H. Campbell, Timothy Wadhams, Karen T. Berger, Shann J. Rufer
Publikováno v:
42nd AIAA Thermophysics Conference.
In an experimental study to obtain detailed heating data over the Space Shuttle Orbiter, CUBRC has completed an extensive matrix of experiments using three distinct models and two unique hypervelocity wind tunnel facilities. This detailed data will b