Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Kurtis R. Long"'
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dfe15c67adf6444caad3cbcc0c012652
https://doi.org/10.2514/6.2017-1279
https://doi.org/10.2514/6.2017-1279
Publikováno v:
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
A hybrid transition trip-dot sizing and placement test technique was developed in support of recent experimental research on a hybrid wing-body configuration under study for the NASA Environmentally Responsible Aviation project. The approach combines
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c451d45b463da75c8207a5480b21dbc5
https://doi.org/10.2514/6.2016-3981
https://doi.org/10.2514/6.2016-3981
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
This paper describes the process used for estimating flow-through balance momentum tares. The interaction of jet engine exhausts on the BOEING/ERA Hybrid Wing Body (HWB) was simulated in the NFAC 40x80 wind tunnel at NASA Ames using a pair of turbine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::52b2475864c82556a89c9e7d27dd49df
https://doi.org/10.2514/6.2016-0265
https://doi.org/10.2514/6.2016-0265
Autor:
James M. Luckring, Ben Nikaido, Joseph A. Garcia, Robert Childs, Dan D. Vicroy, Melissa B. Carter, Michael J. Schuh, Paul Stremel, Jeffrey D. Flamm, Karen A. Deere, Kevin D. James, John E. Melton, Kurtis R. Long
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
NASAs Environmentally Responsible Aviation (ERA) Project explores enabling technologies to reduce aviations impact on the environment. One research challenge area for the project has been to study advanced airframe and engine integration concepts to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::334469dff0999c37ba68109a4dd36014
https://doi.org/10.2514/6.2016-0262
https://doi.org/10.2514/6.2016-0262
Autor:
Patrick R. Shea, Kevin D. James, Michael D. Beyar, Jeffrey D. Flamm, Kurtis R. Long, Daniel M. Tompkins
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Propulsion airframe integration testing on a 5.75% scale hybrid wing body model us- ing turbine powered simulators was completed at the National Full-Scale Aerodynamics Complex 40- by 80-foot test section. Four rear control surface con gurations incl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::26365de63f5895bf965481e293a228b6
https://doi.org/10.2514/6.2016-0011
https://doi.org/10.2514/6.2016-0011
Publikováno v:
Journal of Aerospace Computing, Information, and Communication. 9:110-124
An adaptive scattered data approximation scheme was developed to calibrate the Flush Air Data System (FADS) of a surface vessel. An array of pressure sensors were mounted flush with the deckhouse periphery and the airdata parameters were extracted fr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa1c60426ebabd6dbbccfbb6f806e918
https://doi.org/10.2514/1.54947
https://doi.org/10.2514/1.54947
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
Thermocouples are rugged, compact, and simple temperature sensors that are used in measurements of total temperature in gas turbine engines. However, they are generally considered to have inherently low accuracy. This can be a problem as derived para
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c844ecb67734ed1c63962339420effb
https://doi.org/10.2514/6.2015-4197
https://doi.org/10.2514/6.2015-4197
Publikováno v:
52nd Aerospace Sciences Meeting.
A MEMS floating element shear stress sensor array has been tested under a turbulent boundary layer in an 38 x 38 cm test-section inflow wind tunnel. The MEMS sensor itself is a 1 cm 2 chip with 256 nickel floating elements arrayed in parallel. Real t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::461f1fb8078d2964b05fbfe18d87467d
https://doi.org/10.2514/6.2014-1235
https://doi.org/10.2514/6.2014-1235
Autor:
Scott M. Murman, Kurtis R. Long, Randolph P. Lillard, James C. Ross, Melissa B. Rivers, Michael E. Olsen
Publikováno v:
21st AIAA Computational Fluid Dynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3995fb58fb6e9f4db961d7175417fc77
https://doi.org/10.2514/6.2013-2720
https://doi.org/10.2514/6.2013-2720
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
A small, six sided flush air data system (FADS) anemometer was designed, calibrated, and compared with a maritime ultrasonic anemometer. Design constraints included small size and shape that minimized radar cross section, use of a single absolute pre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3514e89f50e28092d40ce4c11c3b61b0
https://doi.org/10.2514/6.2012-696
https://doi.org/10.2514/6.2012-696