LEADER 00939nam0-2200289---450- 001 990008455890403321 005 20070124120240.0 035 $a000845589 035 $aFED01000845589 035 $a(Aleph)000845589FED01 035 $a000845589 100 $a20070124d1967----km-y0itay50------ba 101 0 $aeng 102 $aUS 105 $aa-------001yy 200 1 $aNose bluntness, cone angle, and mach number effects on the stability derivatives of slender cones$eseptember 1967$fJames T. Clay 210 $aOhio$cAerospace Research Laboratory$d1967 215 $a34 p.$cill.$d28 cm 300 $aSulla cop.: AD 661549 700 1$aClay,$bJames T.$0501932 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008455890403321 952 $aB 69$b351$fDINPA 959 $aDINPA 996 $aNose bluntness, cone angle, and mach number effects on the stability derivatives of slender cones$9728934 997 $aUNINA