Hostname: page-component-78c5997874-t5tsf Total loading time: 0 Render date: 2024-11-10T06:34:10.500Z Has data issue: false hasContentIssue false

Experiments on an aerofoil at high angle of incidence in longitudinal oscillations

Published online by Cambridge University Press:  19 April 2006

C. Maresca
Affiliation:
Institut de Mécanique des Fluides, Laboratoire Associé no. 3 du C.N.R.S., Marseille
D. Favier
Affiliation:
Institut de Mécanique des Fluides, Laboratoire Associé no. 3 du C.N.R.S., Marseille
J. Rebont
Affiliation:
Institut de Mécanique des Fluides, Laboratoire Associé no. 3 du C.N.R.S., Marseille

Abstract

Details of flow visualization, aerodynamic forces and pitching moment, static pressure and skin friction measurements have been carried out on a symmetrical aerofoil at fixed angle of incidence in longitudinal oscillations parallel to the uniform airstream of a wind-tunnel.

This investigation shows weak unsteady effects at incidences below that of static stall. For higher incidences, strong unsteady effects appear and depend on the frequency and amplitude of the oscillations. The measurements indicate an overshoot of the instantaneous lift and drag which is explained by a strong vortex shedding process occurring during the dynamic stall encountered by the aerofoil in decelerated motion, as observed for profiles oscillating in pitch through stall. When the aerofoil is going forward in accelerated motion dynamic reattachment may be observed at very high incidence over a short part of the period of oscillation.

Dynamic stall and dynamic reattachment contribute to a favourable effect of unsteadiness on the mean lift coefficient, which increases as compared to the steady state one, and which is expressed through an empirical formula involving incidence, frequency and amplitude of oscillations. At given incidence, optimization of this feature is achieved by matching the frequency and the amplitude of oscillation, respectively with the frequency linked with the highest peak of energy in the wake, and with the distance between two consecutive vortices in the mean wake when modelled as a von Kármán's vortex street.

Type
Research Article
Copyright
© 1979 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Carr, L. W., Mcalister, K. W. & Mccroskey, W. J. 1977 Analysis of the development of dynamic stall based on oscillating airfoil experiments. N.A.S.A. Tech. Note D-8382.
Comolet, R. 1976 Dynamique des Fluides Réels (2nd edition, ed. Masson), p. 227.
Mccroskey, W. J. & Fisher, R. K. 1972 Detailed aerodynamic measurements on a model rotor in the blade stall regime. J. Amer. Hel. Soc. 17, 1, 20.Google Scholar
Mccroskey, W. J. 1977 Some current research in unsteady fluid dynamics. The 1976 Freeman Scholar Lecture. Trans. A.S.M.E. J. Fluids Engng. 99, 8.Google Scholar
Maresca, C., Rebont, J. & Valensi, J. 1975 Separation on reattachment of the boundary layer on a symmetrical aerofoil oscillating at fixed incidence in a steady flow. In Proc. Univ. Arizona/USAF OSR Symp. Unsteady Aerodynamics ed. R. B. Kinney), vol. 1, p. 35.
Maresca, C., Rebont, J. & Valensi, J. 1976 Caractéristiques aérodynamiques d'un profil en mouvement instationnaire. In IUTAM 14th Int. Cong. Theor. Appl. Mech., Delft. Springer.
Pierce, G. A., Kunz, D. L. & Malone, J. B. 1976 The effect of varying freestream velocity on dynamic stall characteristics. In 32nd Ann. Nat. V/Stol Forum Amer. Hel. Soc. Washington D.C.
Rebont, J., Maresca, C., Guilerminet, A. & Favier, D. 1975 Etude expérimentale relative à 1’aérodynamique d'un rotor d'hélicoptére en vol de translation. In Proc. 12iéme Coll. Aérodyn. Appl. ENSMA CEAT, Poitiers.
Rebont, J., Maresca, C., Favier, D. & Valensi, J. 1977 Recollement dynamique sur un profil d'aile en mouvement de tamis. Influence des paramètres d'oscillation. In Proc. AGARD-FDP Meeting Unsteady Aerodyn., Ottawa.
Roshko, A. 1955 On the wake and drag of bluff bodies. J. Aero. Soc. 22, 2, 124.Google Scholar
Saxena, L. S., Fejer, A. A. & Morkovin, M. V. 1977 Features of unsteady flow over airfoils. In Proc. AGARD-FDP Meeting Unsteady Aerodyn., Ottawa.
Valensi, J. & Rebont, J. 1972 Efforts aérodynamiques sur un profil d'aile animé d'un mouvement harmonique parallèle à 1’écoulement. In Proc. AGARD-FDP Meeting Aérodyn. Rotary Wing, Marseille.