Drag reduction through distributed electric propulsion

AIAA AVIATION 2014 -14th AIAA Aviation Technology, Integration, and Operations Conference

Volumn , Issue , 2014, Pages

  Stoll, Alex M ^a   Bevirt, Joe Ben ^a   Moore, Mark D ^b   Fredericks, William J ^b   Borer, Nicholas K ^b  

^a Joby Energy Inc   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AVIATION; DRAG; LIFT; NAVIER STOKES EQUATIONS; PROPULSION;

DYNAMIC PRESSURES; ELECTRIC AIRCRAFTS; GENERAL AVIATION; LANDING CONDITIONS; MAXIMUM LIFT COEFFICIENT; PROPELLER DESIGN; PROPULSION TECHNOLOGY; SIMILAR ANALYSIS;

WINGS;

EID: 85085401276     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2014-2851     Document Type: Conference Paper

References (6)

1. Kohlman, D. L., Flight Test Results for an Advanced Technology Light Airplane, Journal of Aircraft, Vol. 16, No. 4, April 1979, pp. 250-255.
2. Cirrus Aircraft, 4515 Taylor Circle, Duluth, MN 55811, Airplane Information Manual for the Cirrus Design SR22, Sept. 2011.
3. Cirrus Aircraft, http://cirrusaircraft.com/sr22/, May 2014.
4. Moore, M. D. and Fredericks, W. J., Misconceptions of Electric Aircraft and their Emerging Aviation Markets, AIAA SciTech, American Institute of Aeronautics and Astronautics, Jan. 2014.
5. Holmes, B. J., Flight Evaluation of an Advanced Technology Light Twin-Engine Airplane (ATLIT), NASA CR-2832, July 1977.
6. Patterson, M. D., German, B. J., and Moore, M. D., Performance Analysis and Design of On-Demand Electric Aircraft Concepts, Aviation Technology, Integration, and Operations (ATIO) Conferences, American Institute of Aeronautics and Astronautics, Sept. 2012.