메뉴 건너뛰기




Volumn 1, Issue , 2008, Pages 112-125

Design and testing of a shrouded rotor micro air vehicle with anti-torque vanes

Author keywords

[No Author keywords available]

Indexed keywords

A-CARBON; AERIAL VEHICLES; AXISYMMETRIC; BAR PROFILE; CROSS COUPLINGS; MICRO-AIR-VEHICLE; PAYLOAD CAPABILITIES; ROTOR DOWNWASH; ROTOR TORQUE; STABILIZER BAR; YAW RESPONSE;

EID: 50249146807     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (25)

References (13)
  • 1
    • 2342484310 scopus 로고
    • Ducted Propellers - A critical review of the state of the Art
    • Pergamon Press, New York
    • Sacks, A. and Burnell, J., "Ducted Propellers - A critical review of the state of the Art," Progress in Aeronautical sciences, Vol 3, Pergamon Press, New York, 1962.
    • (1962) Progress in Aeronautical sciences , vol.3
    • Sacks, A.1    Burnell, J.2
  • 2
    • 4143130961 scopus 로고
    • The 'Fenestron' - A shrouded tail rotor concept for helicopters
    • Washington, DC
    • nd Annual Forum Washington, DC, 1986, pp. 597-606.
    • (1986) nd Annual Forum , pp. 597-606
    • Mouille, R.1    Dambra, F.2
  • 3
    • 50249169786 scopus 로고    scopus 로고
    • Effects of shroud geometry on the hover performance of a MAV-scale Shrouded rotor
    • Chandler, AZ, January
    • Pereira, J. and Chopra, I., "Effects of shroud geometry on the hover performance of a MAV-scale Shrouded rotor," AHS International Specialists Meeting on Unmanned Rotorcraft, Chandler, AZ, January, 2005.
    • (2005) AHS International Specialists Meeting on Unmanned Rotorcraft
    • Pereira, J.1    Chopra, I.2
  • 4
    • 0035780657 scopus 로고    scopus 로고
    • Effects of the shroud on aerodynamic performance in helicopter shrouded tail rotor system
    • Xu, G. and Wang, S., "Effects of the shroud on aerodynamic performance in helicopter shrouded tail rotor system," Aircraft Engineering and Aerospace Technology, Vol. 73, No.6, 2001, pp. 568-572
    • (2001) Aircraft Engineering and Aerospace Technology , vol.73 , Issue.6 , pp. 568-572
    • Xu, G.1    Wang, S.2
  • 5
    • 50249166496 scopus 로고    scopus 로고
    • Lipera,L., MicroCraft Ducted Air Vehicle, Micro Craft Inc., San Diego, Internal Report, 2001.
    • Lipera,L., "MicroCraft Ducted Air Vehicle," Micro Craft Inc., San Diego, Internal Report, 2001.
  • 6
    • 0031677525 scopus 로고    scopus 로고
    • th American Helicopter
    • May
    • th American Helicopter Society, May 1998, pp. 1410-1418.
    • (1998) Society , pp. 1410-1418
    • Walsh, D.1    Cycon, J.P.2
  • 7
    • 50249138705 scopus 로고    scopus 로고
    • Hrishikeshavan, V., Sirohi.J., Tishchenko.M., and Chopra, I., Design and Stability of a Shrouded Rotor Micro Air Vehicle with Anti-Torque Vanes, AHS International Specialists' Meeting on Unmanned Rotorcraft, Chandler, Arizona, January, 2007.
    • Hrishikeshavan, V., Sirohi.J., Tishchenko.M., and Chopra, I., "Design and Stability of a Shrouded Rotor Micro Air Vehicle with Anti-Torque Vanes," AHS International Specialists' Meeting on Unmanned Rotorcraft, Chandler, Arizona, January, 2007.
  • 9
    • 34548131636 scopus 로고    scopus 로고
    • Hover performance of a Micro air Vehicle: Rotors at Low Reynolds Number
    • American Helicopter Society
    • Hein, B., and Chopra, I., "Hover performance of a Micro air Vehicle: Rotors at Low Reynolds Number," Journal - American Helicopter Society, 2007.
    • (2007) Journal
    • Hein, B.1    Chopra, I.2
  • 11
    • 20744443751 scopus 로고    scopus 로고
    • Analysis and design of airfoils for use at ultra low Reynolds numbers
    • Kunz, P. and Kroo, I., "Analysis and design of airfoils for use at ultra low Reynolds numbers," Progress in Astronautics and Aeronautics, Vol. 195, pp. 35-60, 2001.
    • (2001) Progress in Astronautics and Aeronautics , vol.195 , pp. 35-60
    • Kunz, P.1    Kroo, I.2
  • 12
    • 85003260074 scopus 로고
    • Dynamic analysis of the Rigid Rotor System
    • May-June
    • Azuma, A., "Dynamic analysis of the Rigid Rotor System," J. Aircraft, vol. 4, no.3, May-June, 1967, pp 203-210.
    • (1967) J. Aircraft , vol.4 , Issue.3 , pp. 203-210
    • Azuma, A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.