000 00599 a2200241 4500
001 275287
020 _a
041 _aeng
080 _aLNASA CR 4008 : 1986
245 _aEffect of aspect ratio on sidewall boundary layer influence in two dimensional airfoil testing
250 _a
260 _aWashington, D.C.
260 _bNational Aeronautics and Space Adminstration
260 _c1986
300 _a32 p.
300 _c
856 _u
490 _aNASA CR 4008 : 1986
700 _a
650 _a
650 _aAirfoil testing, Wind tunnel testing, Wall interference
942 _cPP
942 _2UDC
999 _c232620
_d232620