000 | 00699 a2200241 4500 | ||
---|---|---|---|
001 | 284810 | ||
020 | _a | ||
041 | _aeng | ||
080 | _aLNASA TP 1324 : 1978 | ||
245 | _aLow-speed aerodynamic characteristics of a 16-percent-thick variable-geometry airfoil designed for general aviation applications | ||
250 | _a | ||
260 | _aWashington, D.C. | ||
260 | _bNational Aeronautics & Space Administration | ||
260 | _c1978 | ||
300 | _a74 p. | ||
300 | _c | ||
856 | _u | ||
490 | _aNASA TP 1324 : 1978 | ||
700 | _a | ||
650 | _a | ||
650 | _aLow-speed airfoil section, Reynolds number effects, Experimental-theoretical, General aviation aircraft, GA (PC)-l airfoil | ||
942 | _cPP | ||
942 | _2UDC | ||
999 |
_c244122 _d244122 |