Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Michelle L. Mason"'
Publikováno v:
Journal of Spacecraft and Rockets. 58:38-53
The U.S. Air Force Research Laboratory/U.S. Air Force Office of Scientific Research has sponsored the Boundary Layer Transition (BOLT) experiment to investigate hypersonic boundary-layer transition...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::106729fb7a624b52c6c0153b47a1d93f
https://doi.org/10.2514/1.a34803
https://doi.org/10.2514/1.a34803
Autor:
Emily R. Davis, Michelle L. Mason, Giovanni Salazar, Scott A. Berry, Lucas Agricola, Greg McGowan
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::03f06253955008deb69083f30c4256ce
https://doi.org/10.2514/6.2021-3142
https://doi.org/10.2514/6.2021-3142
Autor:
Scott A. Berry, Rudy A. King, Francis A. Greene, Michelle L. Mason, Elizabeth F. Rieken, Kevin Basore
Publikováno v:
AIAA Scitech 2019 Forum.
A review is provided of recent aerothermodynamic ground-test contributions by NASA Langley Research Center (LaRC) to the BOLT flight test program. Several test entries into the Langley Aerothermodynamic Laboratory 20-Inch Mach 6 Air Tunnel are discus
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b888e63e6c23ea16401e557242cfa986
https://doi.org/10.2514/6.2019-0091
https://doi.org/10.2514/6.2019-0091
Autor:
Scott A. Berry, Michelle L. Mason
Publikováno v:
Journal of Spacecraft and Rockets. 53:678-692
The effects of the fin leading-edge radius and sweep angle on peak heating rates due to shock–shock interactions were investigated in the NASA Langley Research Center 20-Inch Mach 6 Air Tunnel. The cylindrical leading-edge models, with radii varied
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d5d3eaabe2d62c54839b8c04f8de8e7
https://doi.org/10.2514/1.a33434
https://doi.org/10.2514/1.a33434
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8a2924edef261161bb96c21919da758d
https://doi.org/10.2514/6.2016-4322
https://doi.org/10.2514/6.2016-4322
Autor:
Michelle L. Mason, Scott A. Berry
Publikováno v:
45th AIAA Thermophysics Conference.
The effects of fin leading-edge radius and sweep angle on peak heating rates due to shock-shock interactions were investigated in the NASA Langley Research Center 20-Inch Mach 6 Air Tunnel. The cylindrical leading-edge fin models, with radii varied f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9610a490cf1f81443da508f3d8cadd74
https://doi.org/10.2514/6.2015-3109
https://doi.org/10.2514/6.2015-3109
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.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::040a58a00d49b6d19959a2c1f1ebc2fa
https://doi.org/10.2514/6.2015-0213
https://doi.org/10.2514/6.2015-0213
Publikováno v:
Historian; Fall2018, Vol. 80 Issue 3, p635-681, 47p
Publikováno v:
ASHA; Mar95, Vol. 37 Issue 3, p28, 13p