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Volumn , Issue , 1997, Pages

A hybrid anti-icing ice protection system

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ATMOSPHERIC TEMPERATURE; FIGHTER AIRCRAFT; FREEZING; HORIZONTAL STABILIZERS; HYBRID SYSTEMS; NASA; SNOW AND ICE REMOVAL;

EID: 84982318765     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (30)

References (12)
  • 1
    • 3242829667 scopus 로고    scopus 로고
    • Characteristics of Surface Roughness Associated With Leading Edge Ice Accretion
    • Shin, J., "Characteristics of Surface Roughness Associated With Leading Edge Ice Accretion," AIAA Paper № 94-0799.
    • AIAA Paper
    • Shin, J.1
  • 3
    • 0027701991 scopus 로고
    • Aerodynamic Performance Effects due to small Leading-Edge Ice (Roughness) on Wings and Tails
    • Nov.-Dec
    • Valarezo, W.O., and Lynch, FT., and McGhee, R.J., "Aerodynamic Performance Effects due to small Leading-Edge Ice (Roughness) on Wings and Tails," Journal of Aircraft, Vol. 30, № 6, Nov.-Dec., 1993.
    • (1993) Journal of Aircraft , vol.30 , Issue.6
    • Valarezo, W.O.1    Lynch, F.T.2    McGhee, R.J.3
  • 4
    • 84983100821 scopus 로고    scopus 로고
    • Full-Scale Empennage Wind Tunnel Test to Evaluate Effects of Simulated Ice on Aerodynamic Characteristics
    • Ferguson, S., Mullins, B., Smith, D., and Korkan, K., "Full-Scale Empennage Wind Tunnel Test to Evaluate Effects of Simulated Ice on Aerodynamic Characteristics," AIAA Paper № 95-0451.
    • AIAA Paper
    • Ferguson, S.1    Mullins, B.2    Smith, D.3    Korkan, K.4
  • 5
    • 84983115289 scopus 로고    scopus 로고
    • Effects of Icing on the Aerodynamics of a Flapped Airfoil
    • Mullins, B., Smith, D., and Korkan, K., "Effects of Icing on the Aerodynamics of a Flapped Airfoil," AIAA Paper № 95-0449.
    • AIAA Paper
    • Mullins, B.1    Smith, D.2    Korkan, K.3
  • 6
    • 84983100817 scopus 로고
    • British Patent Specification № 505,433 issued to Rudolf Goldschmidt; May 5
    • British Patent Specification № 505,433 issued to Rudolf Goldschmidt; May 5, 1939.
    • (1939)
  • 7
    • 79952463851 scopus 로고
    • USSR Electric Impulse De-Icing System Design
    • July
    • Levin, I.A., ‘USSR Electric Impulse De-Icing System Design,' Aircraft Engineering, p 7, July 1972.
    • (1972) Aircraft Engineering , pp. 7
    • Levin, I.A.1
  • 10
    • 84983189230 scopus 로고    scopus 로고
    • Surface Roughness Due to Residual Ice in the Use of Low Power Deicing Systems
    • Shin, J., and Bond, T., "Surface Roughness Due to Residual Ice in the Use of Low Power Deicing Systems," AIAA Paper № 93-0031.
    • AIAA Paper
    • Shin, J.1    Bond, T.2
  • 11
    • 0342296182 scopus 로고    scopus 로고
    • Validation of NASA Thermal Ice Protection Computer Codes, Part 3 - The Validation of ANTICE
    • AI-Khalil, K.M., Horvath, C., Miller, D.R., Wright, W.B., "Validation of NASA Thermal Ice Protection Computer Codes, Part 3 - the Validation of ANTICE," AIAA Paper 97-0051.
    • AIAA Paper
    • Ai-Khalil, K.M.1    Horvath, C.2    Miller, D.R.3    Wright, W.B.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.