<![CDATA[PKK Library Search for 'au:"Jackson, Charlie M."']]>

<![CDATA[PKK Library Search for 'au:"Jackson, Charlie M."']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Jackson%2C%20Charlie%20M.%22&format=rss2 7 0 200 A SEMIGRAPHICAL METHOD OF APPLYING IMPACT THEORY TO AN ARBITRARY BODY TO OBTAIN THE HYPERSONIC AERODYNAMIC CHARACTERISTICS AT ANGLE OF ATTACK AND SIDESLIP [NASA TN D-795] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394254 By Jackson, Charlie M.. Washington, D.C. National Aeronautics and Space Administration 1961 . 18p , Bound With NASA TN D 791-800

Place Hold on A SEMIGRAPHICAL METHOD OF APPLYING IMPACT THEORY TO AN ARBITRARY BODY TO OBTAIN THE HYPERSONIC AERODYNAMIC CHARACTERISTICS AT ANGLE OF ATTACK AND SIDESLIP [NASA TN D-795]

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394254 ESTIMATION OF FLIGHT PERFORMANCE WITH CLOSED-FORM APPROXIMATIONS TO THE EQUATIONS OF MOTION ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=398649 By Jackson,Charlie M. Nasa, Washington, D.C. 1965 . 30 , Bound With Nasa Tr R-221-227,229-230

Place Hold on ESTIMATION OF FLIGHT PERFORMANCE WITH CLOSED-FORM APPROXIMATIONS TO THE EQUATIONS OF MOTION

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=398649 Estimates of minimum energy requirements for range-controlled return of a nonlifting satellite from a circular orbit [NASA TN D-980] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=399188 By Jackson, Charlie M.. Washington, D.C. Nasa 1961 . 33p , Bound With Nasa Tn D-971-979

Place Hold on Estimates of minimum energy requirements for range-controlled return of a nonlifting satellite from a circular orbit [NASA TN D-980]

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=399188 STATIC LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 1.99 OF A LENTICULAR-SHAPED REENTRY VEHICLE ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=400502 By Jackson,Charlie M. Nasa, Washington, D.C. 1960 . 16 , Bound With Nasa Tn D-511-13,515-20

Place Hold on STATIC LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 1.99 OF A LENTICULAR-SHAPED REENTRY VEHICLE

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=400502 A METHOD FOR DETERMINING SURFACE PRESSURES ON BLUNT BODIES OF REVOLUTION AT SMALL ANGLES OF ATTACK IN SUPERSONIC FLOW ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=400793 By Jackson,Charlie M,Sawyer,Wallace C. Nasa, Washington, D.C. 1968 . 102 , Bound With Nasa Tn D-4861-4864,4866-4870

Place Hold on A METHOD FOR DETERMINING SURFACE PRESSURES ON BLUNT BODIES OF REVOLUTION AT SMALL ANGLES OF ATTACK IN SUPERSONIC FLOW

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=400793 NASA Technical Note [NASA TN D-5046]: A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=402330 Washington NASA 1969 . 65p , Bound together NASA TN D-5041 to 5050 | Bound vol. Acc. No. 101134 contains Acc. No. TR16875 to TR16883

Place Hold on NASA Technical Note [NASA TN D-5046]: A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=402330 CHARACTERISTICS AT MACH NUMBER OF 2.03 OF A SERIES OF HAVING VARIOUS SPANWISE DISTRIBUTIONS OF THICKNESS RATIO AND CHORD [NASA TN D-631] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=448338 By Warner, Robins A.. National Aeronautics and Space Administration Washington, D.C. 1960 . 26p , Bound vol. contains with NASA TN D 631-40

Place Hold on CHARACTERISTICS AT MACH NUMBER OF 2.03 OF A SERIES OF HAVING VARIOUS SPANWISE DISTRIBUTIONS OF THICKNESS RATIO AND CHORD [NASA TN D-631]

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