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Volumn 2, Issue , 2009, Pages 1360-1373

Design of the samarai monowing rotorcraft nano air vehicle

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DATA; AIR VEHICLE; ANALYSIS AND SIMULATION; DEFENSE ADVANCED RESEARCH PROJECTS AGENCIES; FIXED WING; FLAPPING WING; FLIGHT STABILITY; FLIGHT VEHICLES; GUIDANCE AND NAVIGATION; LOCKHEED MARTIN; LOW REYNOLDS NUMBER; MASS DISTRIBUTION; RIGID BODY MODELS; ROTARY WING; ROTOR AIRFOILS; TIP JET; TOTAL MASS; URBAN SURVEILLANCE; VEHICLE STABILITY; WIND-TUNNEL TESTING;

EID: 70350496682     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (11)

References (4)
  • 2
    • 78149432054 scopus 로고    scopus 로고
    • Low Reynolds Number Testing of the AG38 Airfoil for the SAMARAI Nano Air Vehicle, Harold Youngren, Chris Kroninger, Steve Jameson and Ming Chang, AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 7-10, 2008
    • Low Reynolds Number Testing of the AG38 Airfoil for the SAMARAI Nano Air Vehicle," Harold Youngren, Chris Kroninger, Steve Jameson and Ming Chang, AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 7-10, 2008


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.