Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Elgin A. Anderson"'
Publikováno v:
Journal of Fluids Engineering. 126:665-670
The evolution of the streamwise momentum flux for two turbulent, plane, parallel jets discharging through slots in a direction normal to a wall was studied both numerically and experimentally. The numerical results, obtained by solving the Reynolds-a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4ff2617534adbf6828db2c6c04b8e242
https://doi.org/10.1115/1.1778717
https://doi.org/10.1115/1.1778717
Publikováno v:
Journal of Aircraft. 40:1107-1114
Running propellers can have a profound effect on the trim and static stability of an airplane. The method most commonly used for determining propeller stability derivatives is based on blade element theory with the axial component of induced velocity
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::990e69e3598b8f655f17c83dc477d642
https://doi.org/10.2514/2.7221
https://doi.org/10.2514/2.7221
Autor:
Elgin A. Anderson, Todd A. Lawton
Publikováno v:
Journal of Aircraft. 40:699-704
The vortices that trail from the wingtips of a large aircraft provide a significant hazard to an aircraft that follows in its wake. The objective is to contribute to the understanding of these vortices by identifying the conditions where an axial vel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1daba8e2bb347eef5f6059b1386cb118
https://doi.org/10.2514/2.3148
https://doi.org/10.2514/2.3148
Publikováno v:
Journal of Fluids Engineering. 125:389-392
The behavior of symmetric parallel jets was investigated experimentally. Two-component hot-wire surveys of the velocity field were performed over a jet region extending from the nozzle plate to a distance seven times the spacing between the nozzles.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::04e231033ba1b7ab703969d3ccbc2fb9
https://doi.org/10.1115/1.1537257
https://doi.org/10.1115/1.1537257
Publikováno v:
Journal of Aircraft. 39:600-608
A closed-form analytic solution for the downwash induced on an aft tail by the main wing of an airplane is presented. This ine nite series solution is based on Prandtl’ s classical lifting-line theory and accounts for the effects of wing planform s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c7adc4f26be7962f3a16f2bcf598e7d9
https://doi.org/10.2514/2.2998
https://doi.org/10.2514/2.2998
Autor:
Robert E. Spall, Elgin A. Anderson
Publikováno v:
Journal of Fluids Engineering. 123:401-406
The flowfield of dual, parallel planar turbulent jets is investigated experimentally using an x-type hot-wire probe and numerically by solving the Reynolds-averaged Navier-Stokes equations. The performance of both differential Reynolds stress (RSM) a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::545db13e496c6221a40d26cd8ea99082
https://doi.org/10.1115/1.1363701
https://doi.org/10.1115/1.1363701
A NUMERICAL STUDY OF BUOYANT, PULSATING EXCHANGE FLOWS THROUGH A VENT IN A THIN HORIZONTAL PARTITION
Autor:
Elgin A. Anderson, Robert E. Spall
Publikováno v:
Numerical Heat Transfer, Part A: Applications. 36:263-272
The dynamics of buoyancy-driven, pulsating exchange flow between compartments separated by a thin, vented, horizontal partition was studied by numerically integrating the unsteady, axisymmetric Navier-Stokes equations. In terms of the flow coefficien
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eaaef5591426bcea5805eb0458ea41ff
https://doi.org/10.1080/104077899274750
https://doi.org/10.1080/104077899274750
Publikováno v:
42nd AIAA Aerospace Sciences Meeting and Exhibit.
* Currently Research Engineer, Lockheed Martin Missile and Fire Control Orlando. Senior Member AIAA. † Professor, Mechanical and Aerospace Engineering Department. Member AIAA. Abstract The low-speed lateral stability derivatives for a conventional
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4326c248f2026b8ad7451190d900842
https://doi.org/10.2514/6.2004-12
https://doi.org/10.2514/6.2004-12
Autor:
Elgin A. Anderson
Publikováno v:
41st Aerospace Sciences Meeting and Exhibit.
The flow behavior of asymmetric parallel jets was investigated experimentally. Two-component hot wire surveys of the velocity field were performed over a jet region extending from the nozzle plate to a distance 10 times the larger nozzle width. The o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e5cd2f6806c223413cb0dbdade6bed35
https://doi.org/10.2514/6.2003-638
https://doi.org/10.2514/6.2003-638
Publikováno v:
40th AIAA Aerospace Sciences Meeting & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ba08dafaa485e760a374f889bfde4699
https://doi.org/10.2514/6.2002-730
https://doi.org/10.2514/6.2002-730