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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1998, Vol. 19 ›› Issue (1): 6-12.
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Lü Zhiyong, Yang Xiaofeng
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Abstract:
Force measurement results of oscillating delta wings at angle of attack ranging from 0°~90° are presented. Furthermore, effects of leading edge swept angle, oscillating frequency and axle location about which a delta wing oscillates on normal coefficient of the delta wing are given and the mechanism of the effect is discussed.
Key words: oscillating delta wing, patter n, aerodynamics char acteristics, high angle of atta ck, time scale
CLC Number:
V211.41
V211.7
Lü Zhiyong;Yang Xiaofeng. DYNAMIC AERODYNAMIC CHARACTERISTICS AND ANALYSIS OF PARAMETER EFFECT OF OSCILLATING DELTA WINGS[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1998, 19(1): 6-12.
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