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Information Journal Paper

Title

A NEW METHOD FOR PREDICTING THE AMPLITUDE AND FREQUENCY OF A HIGHLY SWEPT WING UNDERGOING ROCKING MOTION

Pages

  175-185

Keywords

Not Registered.

Abstract

 Wing rock motion can be described as an oscillatory bank angle buildup to a constant amplitude rocking motion. This phenomenon is realized for delta wings with more than 74 degrees leading edge sweep angles. where asymmetric vortex shedding occurs before vortex breakdown. For wings with sweep angles less than 74 degrees. rocking motion occurs if the wing is in a yawed situation. In this paper, a new and simple method has been presented to predict the amplitude and frequency of oscillation of delta wings undergoing rocking motion at high angles of attack. The predicted data are in excellent agreement with those obtained by experimental studies for wings with sweep angles of 76 and 80 degrees.

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    APA: Copy

    SOLTANI, M.R., EBRAHIMI, A., & DAVARI, A.R.. (2003). A NEW METHOD FOR PREDICTING THE AMPLITUDE AND FREQUENCY OF A HIGHLY SWEPT WING UNDERGOING ROCKING MOTION. SCIENTIA IRANICA, 10(2), 175-185. SID. https://sid.ir/paper/289462/en

    Vancouver: Copy

    SOLTANI M.R., EBRAHIMI A., DAVARI A.R.. A NEW METHOD FOR PREDICTING THE AMPLITUDE AND FREQUENCY OF A HIGHLY SWEPT WING UNDERGOING ROCKING MOTION. SCIENTIA IRANICA[Internet]. 2003;10(2):175-185. Available from: https://sid.ir/paper/289462/en

    IEEE: Copy

    M.R. SOLTANI, A. EBRAHIMI, and A.R. DAVARI, “A NEW METHOD FOR PREDICTING THE AMPLITUDE AND FREQUENCY OF A HIGHLY SWEPT WING UNDERGOING ROCKING MOTION,” SCIENTIA IRANICA, vol. 10, no. 2, pp. 175–185, 2003, [Online]. Available: https://sid.ir/paper/289462/en

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