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Volumn , Issue , 1997, Pages

Optimization of segmented flaps for in-flight transonic performance enhancement

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYERS; DRAG REDUCTION; FLOW SEPARATION; LINEAR ACTUATORS; NAVIER STOKES EQUATIONS; NUMERICAL METHODS; OPTIMIZATION; SUPERSONIC AIRCRAFT;

EID: 84982318301     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (15)
  • 1
    • 0025056224 scopus 로고
    • The Development and Design Integration of a Variable Camber Wing for Long/Medium Range Aircraft
    • Nov
    • Greff, E., "The Development and Design Integration of a Variable Camber Wing for Long/Medium Range Aircraft, Aeronautical Journal, Nov. 1990, pp. 301-312.
    • (1990) Aeronautical Journal , pp. 301-312
    • Greff, E.1
  • 10
    • 0010366922 scopus 로고
    • patent application NGC № P-l(10193)
    • Arena, A. "Linear Actuator System," patent application NGC № P-l(10193), 1995.
    • (1995) Linear Actuator System
    • Arena, A.1
  • 11
    • 85003347172 scopus 로고
    • Method for Designing Closed Airfoils for Arbitrary Supercritical Speed Distributions
    • October
    • Volpe, G. and Melnik, R., "Method for Designing Closed Airfoils for Arbitrary Supercritical Speed Distributions," Journal of Aircraft. Vol. 23, № 10, October 1986.
    • (1986) Journal of Aircraft , vol.23 , Issue.10
    • Volpe, G.1    Melnik, R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.