000 00636 a2200241 4500
001 280088
020 _a
041 _aeng
080 _aLNASA CR 4042 : 1987
245 _aSimplified fourwall interference assessment procedure for airfoil data obtained in the langley 0.3-meter transonic cryogenic tunnel
250 _a
260 _aWashington, D.C.
260 _bNational Aeronautics and Space Adminstration
260 _c1987
300 _a60 p.
300 _c
856 _u
490 _aNASA CR 4042 : 1987
700 _a
650 _a
650 _aAirfoil testing, Wind tunnel testing, Wall interference
942 _cPP
942 _2UDC
999 _c239541
_d239541