Zobrazeno 1 - 10
of 13
pro vyhledávání: '"James L. Felder"'
Autor:
Arijit Banerjee, Yuyao Wang, Kiruba S. Haran, Dongsu Lee, Matthew J. Starr, Samith Sirimanna, Nathaniel J. Renner, James L. Felder, Aaron D. Anderson, Shivang Agrawal
Publikováno v:
2018 AIAA/IEEE Electric Aircraft Technologies Symposium.
An important thrust in current aerospace research is aircraft electrification, including propulsion system electrification. For an electrified propulsion system to provide net benefit over conventional propulsion, high specific power, power density,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f9392bd0d78e4903c3549b307d449e5b
https://doi.org/10.2514/6.2018-4983
https://doi.org/10.2514/6.2018-4983
Publikováno v:
2018 AIAA/IEEE Electric Aircraft Technologies Symposium.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8764cda0ae4cd6ccbb92e85c1f765290
https://doi.org/10.2514/6.2018-4984
https://doi.org/10.2514/6.2018-4984
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
NASA is investing in Electrified Aircraft Propulsion (EAP) research as part of the portfolio to improve the fuel efficiency, emissions, and noise levels in commercial transport aircraft. Turboelectric, partially turboelectric, and hybrid electric pro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::96b073ffed23bdf9f5800bd727d9a555
https://doi.org/10.2514/6.2017-4701
https://doi.org/10.2514/6.2017-4701
Publikováno v:
Aircraft Engineering and Aerospace Technology. 86:558-561
Purpose – The purpose of this article is to present a summary of recent study results on a turboelectric distributed propulsion vehicle concept named N3-X. Design/methodology/approach – The turboelectric distributed propulsion system uses multipl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bf5cc55594845479dc49d362f990f70f
https://doi.org/10.1108/aeat-04-2014-0037
https://doi.org/10.1108/aeat-04-2014-0037
Autor:
Jason R. Welstead, James L. Felder
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
A single-aisle commercial transport concept with a turboelectric propulsion system architecture was developed assuming entry into service in 2035 and compared to a similar technology conventional configuration. The turboelectric architecture consiste
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7835747c18065ffe0ffebb86aa42dd48
https://doi.org/10.2514/6.2016-1027
https://doi.org/10.2514/6.2016-1027
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
The purpose of this paper is to propose specific power and efficiency as the key performance parameters for a turboelectric aircraft power system and investigate their impact on the overall aircraft. Key functional requirements are identified that im
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ba3b0f40410c848fcfecd6d0dcff9f27
https://doi.org/10.2514/6.2015-3890
https://doi.org/10.2514/6.2015-3890
Autor:
James L. Felder
The civil rights movement in South Carolina has an epic and tumultuous history, beginning with the very first statewide meeting of the NAACP in 1939.With stories of sit-ins, movements and the integration of state universities, this is the first compr
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In a previous study by the authors it was shown that the N3-X, a 300 passenger hybrid wing body (HWB) aircraft with a turboelectric distributed propulsion (TeDP) system, was able to meet the NASA Subsonic Fixed Wing (SFW) project goal for N+3 generat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::000bd41d600bcacb97c1e7b602956518
https://doi.org/10.2514/6.2012-3701
https://doi.org/10.2514/6.2012-3701
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Ideally, standard fan/engine designs can directly be embedded within the airframe of a vehicle. Unfortunately, doing so causes both performance penalties and structural challenges due to boundary layer flow ingested into the propulsors. For the prese
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f568f9ed09d0bf257ce8eb7c875da83a
https://doi.org/10.2514/6.2012-3702
https://doi.org/10.2514/6.2012-3702
Autor:
James L. Felder, Hyun Dae Kim
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
The performance benefit of boundary layer or wake ingestion on marine and air vehicles has been well documented and explored. In this article, a quasi-one-dimensional boundary layer ingestion (BLI) benefit analysis for subsonic and transonic propulsi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bc486dacea692734735bd7e3056e8beb
https://doi.org/10.2514/6.2011-222
https://doi.org/10.2514/6.2011-222