메뉴 건너뛰기




Volumn 35, Issue , 2003, Pages 11-21

Aircraft icing

Author keywords

Certification; Flight safety; Ice formation; Icing codes; Simulation

Indexed keywords

AIRCRAFT; COSTS; ICE;

EID: 0344272182     PISSN: 00664189     EISSN: None     Source Type: Book Series    
DOI: 10.1146/annurev.fluid.35.101101.161217     Document Type: Article
Times cited : (264)

References (38)
  • 1
    • 30744448315 scopus 로고    scopus 로고
    • Ice accretions and icing effects for modern airfoils
    • Addy HE. 2000a. Ice accretions and icing effects for modern airfoils. Tech. Pap. 210031
    • (2000) Tech. Pap. 210031
    • Addy, H.E.1
  • 2
    • 0345299763 scopus 로고    scopus 로고
    • A wind tunnel study of icing effects on a natural laminar flow airfoil
    • Addy HE Jr. 2000b. A wind tunnel study of icing effects on a natural laminar flow airfoil. AIAA-0095
    • (2000) AIAA-0095
    • Addy Jr., H.E.1
  • 3
    • 0344868482 scopus 로고    scopus 로고
    • Validation of thermal ice protection computer codes: Part 3. The validation of ANTICE
    • Al-Khalil KM. 1997. Validation of thermal ice protection computer codes: Part 3. The validation of ANTICE. AIAA-0051
    • (1997) AIAA-0051
    • Al-Khalil, K.M.1
  • 4
    • 0344436639 scopus 로고    scopus 로고
    • Ice accretion simulation evaluation test
    • Appl. Vehicle Technol. Panel (AVT) Task Group. ed. RJ Kind. Neuilly-Sur-Seine Cedex, France: NATO
    • Appl. Vehicle Technol. Panel (AVT) Task Group. 2001. Ice accretion simulation evaluation test. NATO/RTO TR-038 AC/323(AVT-006) TP/26, ed. RJ Kind. Neuilly-Sur-Seine Cedex, France: NATO
    • (2001) NATO/RTO TR-038 AC/323(AVT-006)TP/26
  • 5
    • 85088001383 scopus 로고
    • Aerodynamic measurements of an airfoil with simulated glaze ice
    • Bragg MB, Coirier WJ. 1986. Aerodynamic measurements of an airfoil with simulated glaze ice. AIAA 86-0484
    • (1986) AIAA 86-0484
    • Bragg, M.B.1    Coirier, W.J.2
  • 7
    • 0345299758 scopus 로고
    • Prediction of the aerodynamic performance degradation of an aircraft in natural icing conditions
    • Cebeci T, Besnard E. 1994. Prediction of the aerodynamic performance degradation of an aircraft in natural icing conditions. AIAA 94- 0487
    • (1994) AIAA 94-0487
    • Cebeci, T.1    Besnard, E.2
  • 9
    • 73649121789 scopus 로고
    • Improvement of the ONERA 3D Icing Code, comparison with 3D experimental shapes
    • Hedde T, Gufford D. 1993. Improvement of the ONERA 3D Icing Code, comparison with 3D experimental shapes. AIAA 93-0169
    • (1993) AIAA 93-0169
    • Hedde, T.1    Gufford, D.2
  • 10
    • 0016128948 scopus 로고
    • The problem of three-dimensional lifting flow and its solution by means of surface singularity distribution
    • Hess JL. 1974. The problem of three-dimensional lifting flow and its solution by means of surface singularity distribution. Comput. Methods Appl. Mech. Eng. 4:283-319
    • (1974) Comput. Methods Appl. Mech. Eng. , vol.4 , pp. 283-319
    • Hess, J.L.1
  • 11
    • 84894327157 scopus 로고    scopus 로고
    • Ice accretion and its effects on aerodynamics of unprotected aircraft components
    • Ottawa, Can
    • Laschka B, Jesse RE. 1997. Ice accretion and its effects on aerodynamics of unprotected aircraft components. AGARD Rep. 127 (Aircraft Icing), Ottawa, Can.
    • (1997) AGARD Rep. 127 (Aircraft Icing)
    • Laschka, B.1    Jesse, R.E.2
  • 14
    • 0344436637 scopus 로고    scopus 로고
    • In-flight icing encounter and uncontrolled collision with terrain
    • Natl. Transp. Safety Board Aviat. Accid. Rep. Monroe, Michigan. NTSB Accid. No. DCA97MA017
    • Natl. Transp. Safety Board Aviat. Accid. Rep. 1997. In-flight icing encounter and uncontrolled collision with terrain, Comair Flight 3272, Embraer EMB-120T, N265CA, Monroe, Michigan. NTSB Accid. No. DCA97MA017
    • (1997) Comair Flight 3272, Embraer EMB-120T, N265CA
  • 15
    • 0022941293 scopus 로고
    • Experimental evidence for modifying the current physical model for ice accretion on aircraft surfaces
    • Olsen WA, Walker E. 1986. Experimental evidence for modifying the current physical model for ice accretion on aircraft surfaces. NASA Tech. Memo. 87184
    • (1986) NASA Tech. Memo. 87184
    • Olsen, W.A.1    Walker, E.2
  • 17
    • 84983208372 scopus 로고    scopus 로고
    • A review of NASA Lewis' development plans for computational simulation of aircraft icing
    • Potapczuk MG. 1999. A review of NASA Lewis' development plans for computational simulation of aircraft icing. NASA Tech. Memo. 208904. AIAA-99-0243
    • (1999) NASA Tech. Memo. 208904. AIAA-99-0243
    • Potapczuk, M.G.1
  • 18
    • 0344436642 scopus 로고    scopus 로고
    • Conjugate heat transfer: Progress on the ice accretion code CANICE
    • Bombardier Aerosp., Montreal, Canada
    • Pueyo A. 2001. Conjugate heat transfer: progress on the ice accretion code CANICE. Adv. Aerodyn. Memo. MAA-000-382. Bombardier Aerosp., Montreal, Canada
    • (2001) Adv. Aerodyn. Memo. MAA-000-382
    • Pueyo, A.1
  • 19
    • 0344436641 scopus 로고    scopus 로고
    • Improvements to the ice accretion code CANICE
    • Ontario, Can.: Can. Aeronaut. Space Inst
    • Pueyo A, Chocron D, Kafyeke F. 2001. Improvements to the ice accretion code CANICE. Proc. CASI Annu. Conf., 48th, pp. 253-61. Ontario, Can.: Can. Aeronaut. Space Inst.
    • (2001) Proc. CASI Annu. Conf., 48th , pp. 253-261
    • Pueyo, A.1    Chocron, D.2    Kafyeke, F.3
  • 20
    • 85040502327 scopus 로고
    • Performance degradation of a typical twin engine commuter type aircraft in measured natural icing conditions
    • Ramando RJ, Mikelson KL, McKnight RC. 1984. Performance degradation of a typical twin engine commuter type aircraft in measured natural icing conditions. NASA Tech. Memo. 83564
    • (1984) NASA Tech. Memo. 83564
    • Ramando, R.J.1    Mikelson, K.L.2    McKnight, R.C.3
  • 21
    • 0344005412 scopus 로고
    • Prediction of ice accretion on a swept NACA 0012 airfoil and comparisons to flight test results
    • Reehorst AL. 1992. Prediction of ice accretion on a swept NACA 0012 airfoil and comparisons to flight test results. AIAA 92-0043
    • (1992) AIAA 92-0043
    • Reehorst, A.L.1
  • 23
    • 2142858049 scopus 로고
    • User manual for the NASA Lewis ice accretion code (LEWICE)
    • Ruff GA, Berkowitz BM. 1990. User manual for the NASA Lewis ice accretion code (LEWICE). NASA CR 185129
    • (1990) NASA CR 185129
    • Ruff, G.A.1    Berkowitz, B.M.2
  • 24
    • 0028396703 scopus 로고
    • Prediction of ice shapes and their effect on airfoil performance
    • Shin J, Berkowitz B, Chen HH, Cebeci T. 1993. Prediction of ice shapes and their effect on airfoil performance. J. Aircr. 31:263-70
    • (1993) J. Aircr. , vol.31 , pp. 263-270
    • Shin, J.1    Berkowitz, B.2    Chen, H.H.3    Cebeci, T.4
  • 25
    • 0009525736 scopus 로고
    • Experimental and computational ice shapes and resulting drag increase for a NACA airfoil
    • 5th, Calif. State Univ., Long Beach
    • Shin J, Bond T. 1992a. Experimental and computational ice shapes and resulting drag increase for a NACA airfoil. Proc. Symp. Numer. Phys. Asp. Aerodyn. Flows, 5th, Calif. State Univ., Long Beach
    • (1992) Proc. Symp. Numer. Phys. Asp. Aerodyn. Flows
    • Shin, J.1    Bond, T.2
  • 26
    • 0343425048 scopus 로고
    • Results of an icing test on a NACA 0012 airfoil in the NASA Lewis icing research tunnel
    • Shin J, Bond T. 1992b. Results of an icing test on a NACA 0012 airfoil in the NASA Lewis icing research tunnel. AIAA Pap. 92-0647
    • (1992) AIAA Pap. 92-0647
    • Shin, J.1    Bond, T.2
  • 27
    • 0344005411 scopus 로고    scopus 로고
    • Icing tunnel testing methodology
    • Ed. Canadian Aeronautics and Space Institute, 1685 Russel Road, Unit 1R, Ottawa, Ontario, Canada K1G ON1
    • Tezok F, Fritz E. 1997. Icing tunnel testing methodology. Proc. CASI Aerodyn. Symp., 6th, pp. 81-100. Ed. Canadian Aeronautics & Space Institute, 1685 Russel Road, Unit 1R, Ottawa, Ontario, Canada K1G ON1
    • (1997) Proc. CASI Aerodyn. Symp., 6th , pp. 81-100
    • Tezok, F.1    Fritz, E.2
  • 30
    • 85051664937 scopus 로고    scopus 로고
    • Numerical simulation of ice accretion on multiple element configurations
    • Tran P, Brahimi MT, Tezok F, Paraschivoiu I. 1996. Numerical simulation of ice accretion on multiple element configurations. AIAA 96- 0869
    • (1996) AIAA 96-0869
    • Tran, P.1    Brahimi, M.T.2    Tezok, F.3    Paraschivoiu, I.4
  • 33
    • 84983168144 scopus 로고    scopus 로고
    • Parametric experimental study of the formation of glaze ice shapes on swept wings
    • Presented at AIAA Aerosp. Sci. Meet., 37th, Reno, NV
    • Vargas M, Reshotko E. 1999. Parametric experimental study of the formation of glaze ice shapes on swept wings. NASA Tech. Memo. 208900, AIAA 99-0094. Presented at AIAA Aerosp. Sci. Meet., 37th, Reno, NV
    • (1999) NASA Tech. Memo. 208900, AIAA 99-0094
    • Vargas, M.1    Reshotko, E.2
  • 34
    • 0344436634 scopus 로고
    • A theoretical and experimental means to predict ice accretion shapes for evaluating aircraft handling and performance characteristics
    • Ottawa, Can
    • Wilder RW, 1977. A theoretical and experimental means to predict ice accretion shapes for evaluating aircraft handling and performance characteristics. AGARD Rep. No. 127 (Aircraft Icing), Ottawa, Can.
    • (1977) AGARD Rep. No. 127 (Aircraft Icing)
    • Wilder, R.W.1
  • 35
    • 0344436640 scopus 로고    scopus 로고
    • Validation of NASA thermal ice protection computer codes part 2 - LEWICE/Thermal
    • Wright WB. 1997. Validation of NASA thermal ice protection computer codes part 2- LEWICE/Thermal. AIAA Pap. 0050
    • (1997) AIAA Pap. 0050
    • Wright, W.B.1
  • 37
    • 0344868479 scopus 로고    scopus 로고
    • User manual for the NASA Glenn ice accretion code LEWICE
    • Wright WB. 1999b. User manual for the NASA Glenn ice accretion code LEWICE. NASA CR 1999-209409
    • (1999) NASA CR 1999-209409
    • Wright, W.B.1
  • 38
    • 0041620234 scopus 로고    scopus 로고
    • Validation results for LEWICE 2.0
    • Presented at AIAA Aerosp. Sci. Meet., 37th, Reno, NV
    • Wright WB, Rutkowski A. 1999. Validation results for LEWICE 2.0. AIAA Pap. 99-0249. Presented at AIAA Aerosp. Sci. Meet., 37th, Reno, NV
    • (1999) AIAA Pap. 99-0249
    • Wright, W.B.1    Rutkowski, A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.