메뉴 건너뛰기




Volumn 36, Issue 2, 1999, Pages 468-471

Wing pitching and loading with propeller interference

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AIRCRAFT PROPELLERS; BOUNDARY ELEMENT METHOD; COMPUTATIONAL METHODS; FLIGHT DYNAMICS; FLUID STRUCTURE INTERACTION; LIFT; STEADY FLOW; VORTEX FLOW; WAKES;

EID: 0344671607     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2455     Document Type: Article
Times cited : (14)

References (24)
  • 1
    • 0029710323 scopus 로고    scopus 로고
    • Aerodynamic interaction study of the propeller/wing different configurations
    • Chiaramonte, J. Y., Favier, D., Maresca, C., and Benneceur, S., "Aerodynamic Interaction Study of the Propeller/Wing Different Configurations," Journal of Aircraft, Vol. 33, No. 1, 1996, pp. 46-53.
    • (1996) Journal of Aircraft , vol.33 , Issue.1 , pp. 46-53
    • Chiaramonte, J.Y.1    Favier, D.2    Maresca, C.3    Benneceur, S.4
  • 3
    • 0025090424 scopus 로고
    • Aerodynamic interactions between propellers and wings
    • Witkowski, D., Lee, A., and Sullivan, J., "Aerodynamic Interactions Between Propellers and Wings," Journal of Aircraft, Vol. 26, No. 9, 1989, pp. 829-836.
    • (1989) Journal of Aircraft , vol.26 , Issue.9 , pp. 829-836
    • Witkowski, D.1    Lee, A.2    Sullivan, J.3
  • 4
    • 0025401017 scopus 로고
    • Propeller-wing interaction using a frequency domain panel method
    • Cho, J., and Williams, M. H., "Propeller-Wing Interaction Using a Frequency Domain Panel Method," Journal of Aircraft, Vol. 27, No. 3, 1990, pp. 196-203.
    • (1990) Journal of Aircraft , vol.27 , Issue.3 , pp. 196-203
    • Cho, J.1    Williams, M.H.2
  • 5
    • 0004698302 scopus 로고
    • Compressible potential flow around a helicopter rotor
    • Springer-Verlag, New York
    • Rottgermann, A., and Wagner, S., "Compressible Potential Flow Around a Helicopter Rotor," Computational Mechanics, Vol. 2, Springer-Verlag, New York, 1995, pp. 2915-2920.
    • (1995) Computational Mechanics , vol.2 , pp. 2915-2920
    • Rottgermann, A.1    Wagner, S.2
  • 6
    • 85038055990 scopus 로고
    • The aerodynamic characteristics of a smooth wing at low reynolds number under effect of a pusher propeller
    • available on CD Rom by Microservice, São Paulo, Brazil
    • Catalano Martini, F., "The Aerodynamic Characteristics of a Smooth Wing at Low Reynolds Number Under Effect of a Pusher Propeller," Proceedings of the 13th Symposium COBEM-C1DIM'95 (Belo Horizonte, Brazil), available on CD Rom by Microservice, São Paulo, Brazil, 1995.
    • (1995) Proceedings of the 13th Symposium COBEM-C1DIM'95 (Belo Horizonte, Brazil)
    • Catalano Martini, F.1
  • 7
    • 0026835936 scopus 로고
    • Boundary element method for the analysis of the unsteady flow around extreme propeller geometries
    • Kinnas, A. S., and Hsin, C. Y., "Boundary Element Method for the Analysis of the Unsteady Flow Around Extreme Propeller Geometries," AJAA Journal, Vol. 30, No. 3, 1992, pp. 688-696.
    • (1992) AJAA Journal , vol.30 , Issue.3 , pp. 688-696
    • Kinnas, A.S.1    Hsin, C.Y.2
  • 8
    • 85002578386 scopus 로고
    • Velocities induced by semi-infinite helical vortex filaments
    • Graber, A., and Rosen, A., "Velocities Induced by Semi-Infinite Helical Vortex Filaments," Journal of Aircraft, Vol. 24. No. 5, 1987, pp. 289, 290.
    • (1987) Journal of Aircraft , vol.24 , Issue.5 , pp. 289
    • Graber, A.1    Rosen, A.2
  • 9
    • 0028262066 scopus 로고
    • Oscillating foils for marine propulsion
    • International Society of Offshore and Polar Engineering, Osaka, Japan
    • Yamaguchi, H., and Bose, N., "Oscillating Foils for Marine Propulsion," Proceedings of the 4th International Offshore and Polar Engineering Conference, Vol. 3, International Society of Offshore and Polar Engineering, Osaka, Japan, 1994, pp. 539-544.
    • (1994) Proceedings of the 4th International Offshore and Polar Engineering Conference , vol.3 , pp. 539-544
    • Yamaguchi, H.1    Bose, N.2
  • 10
    • 0029489706 scopus 로고
    • Performance of chordwise flexible oscillating propulsors using a time-domain panel method
    • Bose, N., "Performance of Chordwise Flexible Oscillating Propulsors Using a Time-Domain Panel Method," International Shipbuilding Progress, Vol. 432, No. 42, 1995, pp. 281-294.
    • (1995) International Shipbuilding Progress , vol.432 , Issue.42 , pp. 281-294
    • Bose, N.1
  • 11
    • 0030195751 scopus 로고    scopus 로고
    • Visualization and measurement of helicopter rotor flow with swept back tip shapes at hover flight using the flow visualization gun time line technique
    • Müller, R. H. G., Nsi Mba, M., Aymard, E., Favier, D., Berton, E., and Maresca, C., "Visualization and Measurement of Helicopter Rotor Flow with Swept Back Tip Shapes at Hover Flight Using the Flow Visualization Gun Time Line Technique," Experiments in Fluids, Vol. 21, No. 3, 1996, pp. 161-169.
    • (1996) Experiments in Fluids , vol.21 , Issue.3 , pp. 161-169
    • Müller, R.H.G.1    Nsi Mba, M.2    Aymard, E.3    Favier, D.4    Berton, E.5    Maresca, C.6
  • 14
    • 0024732222 scopus 로고
    • Numerical and experimental investigation of isolated propeller wakes in axial flight
    • Favier, D., Ettaouil, A., and Maresca, C., "Numerical and Experimental Investigation of Isolated Propeller Wakes in Axial Flight," Journal of Aircraft, Vol. 26, No. 9, 1989, pp. 837-846.
    • (1989) Journal of Aircraft , vol.26 , Issue.9 , pp. 837-846
    • Favier, D.1    Ettaouil, A.2    Maresca, C.3
  • 15
    • 0040790133 scopus 로고
    • Coefficienti di trazione, di coppia e rendimento dell'elica in presenza del campo aerodinamico di un'ala finita
    • Ardito Marretta, R. M., and Lombardo, G., "Coefficienti di Trazione, di Coppia e Rendimento dell'Elica in Presenza del Campo Aerodinamico di un'Ala Finita," Aerotecnica-Missili e Spazio, Vol. 73, Nos. 1-2, 1994, pp. 31-41.
    • (1994) Aerotecnica-Missili e Spazio , vol.73 , Issue.1-2 , pp. 31-41
    • Ardito Marretta, R.M.1    Lombardo, G.2
  • 16
    • 0030246531 scopus 로고    scopus 로고
    • Performance of a propeller embedded in the flowfield of a wing
    • Ardito Marretta, R. M., "Performance of a Propeller Embedded in the Flowfield of a Wing," Journal of Aircraft, Vol. 33, No. 5, 1996, pp. 919-923.
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 919-923
    • Ardito Marretta, R.M.1
  • 18
    • 85038058845 scopus 로고    scopus 로고
    • Hybrid numerical technique for evaluating wing aerodynamic loading with propeller interference
    • to be published
    • Ardito Marretta, R. M., Davi', G., Lombardi, G., and Milazzo, A., "Hybrid Numerical Technique for Evaluating Wing Aerodynamic Loading with Propeller Interference," Computers and Fluids (to be published).
    • Computers and Fluids
    • Ardito Marretta, R.M.1    Davi', G.2    Lombardi, G.3    Milazzo, A.4
  • 19
    • 0030246083 scopus 로고    scopus 로고
    • Lifting-line theory of an arched wing in asymmetric flight
    • Iosilevskii, G., "Lifting-Line Theory of an Arched Wing in Asymmetric Flight," Journal of Aircraft, Vol. 33, No. 5, 1996, pp. 1023-1026.
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 1023-1026
    • Iosilevskii, G.1
  • 21
    • 44949279141 scopus 로고
    • On an extension of prandtl's lifting line theory to curved wings
    • Prossdorf, S., and Tordella, D., "On an Extension of Prandtl's Lifting Line Theory to Curved Wings," Impact of Computing in Science and Engineering, Vol. 3, Nos. 1-3, 1991, pp. 192-212.
    • (1991) Impact of Computing in Science and Engineering , vol.3 , Issue.1-3 , pp. 192-212
    • Prossdorf, S.1    Tordella, D.2
  • 23
    • 0030856719 scopus 로고    scopus 로고
    • Explicit kutta condition for unsteady two-dimensional high-order potential boundary element method
    • Davi', G., Ardito Marretta, R. M., and Milazzo, A., "Explicit Kutta Condition for Unsteady Two-Dimensional High-Order Potential Boundary Element Method," AIAA Journal, Vol. 35, No. 6, 1997, pp. 1080, 1081.
    • (1997) AIAA Journal , vol.35 , Issue.6 , pp. 1080
    • Davi', G.1    Ardito Marretta, R.M.2    Milazzo, A.3
  • 24
    • 0344474804 scopus 로고    scopus 로고
    • High aspect ratio wings: Tip vortex structure and its numerical implications
    • July
    • Lombardi, G., and Cannizzo, F., "High Aspect Ratio Wings: Tip Vortex Structure and Its Numerical Implications," AIAA Paper 96-1961, July 1996.
    • (1996) AIAA Paper 96-1961
    • Lombardi, G.1    Cannizzo, F.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.