01593cam a22003977a 4500001000800000005001700008007001400025008004100039035002000080035001200100037002100112040001300133074001900146086002000165091000800185100002000193245013300213260019100346300000900537490003600546490004500582500005500627500003400682533010700716650002800823650002900851650002100880650003400901650002700935650002500962700002800987710006001015830004001075830004601115984003401161411508120171212145412.0he bmb---bbca960521s1995 cau b f000 0 eng d a(OCoLC)34762345 a4115081 aN 96-11652bNASA aGPObeng a0830-H-14 (MF)0 aNAS 1.26:199151 amfm1 aReuther, James.12aA comparison of design variables for control theory based airfoil optimizationh[microform] /cJames Reuther and Antony Jameson. a[Moffett Field, Calif.] :bResearch Institute for Advanced Computer Science, NASA Ames Research Center ;a[Springfield, Va. :bNational Technical Information Service, distributor,c1995] a1 v.1 aRIACS technical report ;v95.131 aNASA contractor report ;vNASA CR-199151 aDistributed to depository libraries in microfiche. aShipping list no.: 96-0195-M. aMicrofiche.b[Washington, D.C. :cNational Aeronautics and Space Administration,d1995]e1 microfiche. 7aAircraft design.2nasat 7aAirfoil profiles.2nasat 7aAirfoils.2nasat 7aComputer aided design.2nasat 7aControl theory.2nasat 7aOptimization.2nasat1 aJameson, Antony,d1934-2 aResearch Institute for Advanced Computer Science (U.S.) 0aRIACS technical report ;vTR 95-13. 0aNASA contractor report ;vNASA CR-199151. aANLcmc SUDOC NAS 1.26:199151