AIRFOIL TRAILING-EDGE FLOW MEASUREMENTS

被引:45
作者
BROOKS, TF
MARCOLINI, MA
POPE, DS
机构
[1] NASA, LANGLEY RES CTR, HAMPTON, VA 23665 USA
[2] KENTRON INT INC, HAMPTON, VA USA
关键词
D O I
10.2514/3.9426
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:1245 / 1251
页数:7
相关论文
共 9 条
[1]   SCALING OF AIRFOIL SELF-NOISE USING MEASURED FLOW PARAMETERS [J].
BROOKS, TF ;
MARCOLINI, MA .
AIAA JOURNAL, 1985, 23 (02) :207-213
[2]  
BROOKS TF, 1984, AIAA842266 PAP
[3]  
BROOKS TF, 1983, AIAA830785 PAP
[4]  
H. Schlichting, 1968, BOUNDARY LAYER THEOR
[5]  
HARRIS JE, 1982, NASA TM83207
[6]   CALCULATION OF TWO-DIMENSIONAL NEAR AND FAR WAKES [J].
PATEL, VC ;
SCHEUERER, G .
AIAA JOURNAL, 1982, 20 (07) :900-907
[7]   PREDICTION OF THE CHARACTERISTICS OF 2-DIMENSIONAL AIRFOILS [J].
SPENCE, DA .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (09) :577-&
[8]  
VISWANATH PR, 1979, AIAA791503 PAP
[9]  
ZORUMSKI WE, 1982, NASA TM83199