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document
Lee, G.E.M. van der (author), Duel, H. (author), Groot, S. (author), Aarts, H. (author), Pouwels, R. (author)
report 2000
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Lee, C.-H. (author)
conference paper 1999
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Lee, H.H. (author)
journal article 1999
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Lee, C.-H (author), Newman, J.N. (author)
report 1999
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Paik, Jeom Kee (author), Lee, Yong Wook (author), Thayamballi, Anil K. (author), Curry, Robert (author)
report 1997
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Hsueh, W.-J. (author), Lee, Ya-Jung (author)
journal article 1997
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Lee, Charles M. (author)
journal article 1995
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Lee, G.J. (author)
journal article 1995
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Lee, B.S. (author), Vassalos, D. (author)
journal article 1995
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Lee, Seung-Joon (author)
journal article 1995
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Lee, Seok-Won (author)
journal article 1994
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Shankararaman, V. (author), Lee, B.S. (author)
conference paper 1994
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Korsmeyer, F. Thomas (author), Lee, C.-H. (author), Newman, J.N. (author)
journal article 1993
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Lee, Tzung-Hang (author)
report 1992
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Lee, C.H. (author), Newman, J.N. (author)
journal article 1991
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Epstein, M.B. (author), Huber, J.P. (author), Aniol, K.A. (author), Bracco, A. (author), Davis, C.A. (author), Gubler, H.P. (author), Lee, W.P. (author), Margazioti, D.J. (author), Perdrisat, C.F. (author), Poffenberger, P.R. (author), Postma, H. (author), Punjabi, V. (author), Sebel, H.J. (author), Stetz, A.W. (author), van Oers, W.T.H. (author)
journal article 1990
document
Lee, C.-H. (author)
journal article 1989
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Lee, B.B.K. (author), Tang, F.C. (author)
A supercritical airfoil with a trailing edge flap has been the subject of aerodynamic investigation in the National Aeronautical Establishment's High Reynolds Number 2-D Test Facility. The effects of flap deflection on buffet intensities and delay of buffet onset at transonic speeds were studied. Buffet boundaries for various flap angles were...
report 1988
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Lee, Kyu-Yeul (author)
conference paper 1988
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Lee, B.H.K. (author), Desrochers, J. (author)
Nonlinear flutter of a two-dimensional airfoil undergoing plunging and pitching motions is studied using a time marching finite difference scheme. The structural nonlinearity considered is of the type due to a spring with preload and freeplay. Flutter is determined from solutions of the structural dynamic equations of motion when either...
report 1987
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