000 00489pam a2200133a 44500
082 _aNASA
_bTN D-217
100 _aFournier,Paul G
245 1 _aLOW -SPEED INVESTIGATION OF STATIC LONGITUINAL AND LATERAL STABILITY CHRACTERISTICS OF AN AIRPLANE CONFIGURATION WITH A HIGHLY TAPERED WING AND WITH SEVRAL BODY AND TAIL ARRANGMENTS.
260 _a
_bNasa, Washington, D.C.
_c1960
300 _a46
500 _aBound With Nasa Tn D-211-216,218-220.
964 _gCIRC
997 _aTR13108 C
999 _c398412
_d398412