Zobrazeno 1 - 10
of 56
pro vyhledávání: '"Gregory S. Jones"'
Publikováno v:
Journal of Aircraft. 60:32-46
An experimental study is conducted to investigate the effects of upper-surface trailing-edge blowing on a low-aspect-ratio rectangular wing with an actively actuated flap. Two wing configurations, the wing with a baseline flap and a dual-radius flap,
Publikováno v:
Journal of Aircraft. 58:781-792
A wind tunnel test was performed in the 0.3-Meter Cryogenic Transonic Tunnel at the NASA Langley Research Center to investigate the impact of various boundary layer thickeners on the height and sha...
Publikováno v:
SSRN Electronic Journal.
Autor:
Gregory S. Jones
Publikováno v:
The Nonproliferation Review. 26:61-81
The claim that reactor-grade plutonium cannot or will not be used to produce nuclear weapons has been used to justify non-nuclear-weapon states’ large stockpiles of plutonium that has been separate...
Publikováno v:
AIAA Scitech 2021 Forum.
Autor:
Gaetan K. Kenway, William E. Milholen, Michael D. Bozeman, Christopher J. Cramer, Gregory S. Jones, Alaa A. Elmiligui, Christopher M. Cagle
Publikováno v:
AIAA Scitech 2020 Forum.
Publikováno v:
AIAA Scitech 2020 Forum.
A wind tunnel test was performed in the 0.3-Meter Cryogenic Transonic Tunnel at the NASA Langley Research Center to investigate the impact of various boundary layer thickeners on the height and shape of the boundary layer on the aft portion of a semi
Autor:
Gregory S. Jones
Publikováno v:
Mnemosyne. 69:1034-1039
Autor:
C. Mark Cagle, Scott L. Goodliff, William E. Milholen, Jared S. Fell, Gregory S. Jones, David T. Chan
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
The FAST-MAC circulation control model was modified to test an array of steady and unsteady actuators at realistic flight Reynolds numbers in the National Transonic Facility at the NASA Langley Research Center. Previous experiments in the FAST-MAC te
Autor:
William E. Milholen, David T. Chan, Scott L. Goodliff, LaTunia G. Pack Melton, Gregory S. Jones, Christopher M. Cagle
Publikováno v:
35th AIAA Applied Aerodynamics Conference.
The FAST-MAC circulation control model was modified to test an array of unsteady sweeping-jet actuators at realistic flight Reynolds numbers in the National Transonic Facility at the NASA Langley Research Center. Two types of sweeping jet actuators w