Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Craig A. Paxton"'
Publikováno v:
AIAA Journal. 45:2087-2090
T O ACHIEVE revolutionary aircraft performance, advanced technologies should be pursued to drastically reduce the weight of aircraft and fuel consumption and significantly increase aircraft mission payload and maneuverability. Both the military and c
Publikováno v:
Journal of Aircraft. 43:987-995
Two coflowjet airfoils with injection slot size differing by a factor of 2 are tested in a wind tunnel to study the effect of injection slot size. At the same angle of attack, the larger injection slot size airfoil passes about twice the jet mass flo
Autor:
Craig J. Paxton, Richard B. Moss, Terry E. Robinson, Manisha Newaskar, Daniel A. Bloch, Krishnaveni Kesavarju, Samuel Moon-Ho Song, Anne-Sophie Bonnel
Publikováno v:
Pediatric Pulmonology. 38:396-405
The purpose of this study was to compare quantitative computed tomography air trapping (AT) and pulmonary function measurements between subjects with mild cystic fibrosis lung disease (MCF; forced expiratory volume in 1 sec (FEV1)70% predicted) and n
Autor:
Chris M. Vaccarello, Andrew J. Keith, K. Preston White, Renee A. Galione, Matthew Miller, Craig A. Paxton, Mike Smith, Alan C. Fu
Publikováno v:
2011 IEEE Systems and Information Engineering Design Symposium.
The Albemarle-Charlottesville Regional Jail, having been built to house less than the forecasted inmate population, is currently operating at 150% of its rated capacity. The ever growing inmate population has put a strain on the already limited jail
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
*† ‡ § ** The wind tunnel tests reported in this paper demonstrate the ability of the co-flow jet airfoil to dramatically increase lift, stall margin, and drag reduction. Detailed velocity field measurements are reported for a baseline NACA0025
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
Publikováno v:
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Publikováno v:
2nd AIAA Flow Control Conference.
Anovelsubsonicairfoilcirculationaugmenttechniqueusingco-∞owjet(CFJ)toachievesuperioraerodynamicperformanceforsubsonicaircraftisprovednumericallybyCFDsimulation. Theadvantagesofco-∞owjetairfoilincludehighliftathighangleofattack,ultrahigh Cl=Cdat c