<![CDATA[PKK Library Search for 'au:"Suttles,John T."']]>

<![CDATA[PKK Library Search for 'au:"Suttles,John T."']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Suttles%2CJohn%20T.%22&format=rss2 6 0 200 CURVE FITS OF PREDICTED INVISCID STAGNATION-POINT RADIATIVE HEATING RATES, COOLING FACTORS, AND SHOCK STANDOFF DISTANCES FOR HYPERSONIC EARTH ENTRY ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=392860 By Suttles,John T, Sullivan,Edward M. Nasa, Washington, D.C. 1974 . 41 , Bound With Nasa Tn D-7621-30

Place Hold on CURVE FITS OF PREDICTED INVISCID STAGNATION-POINT RADIATIVE HEATING RATES, COOLING FACTORS, AND SHOCK STANDOFF DISTANCES FOR HYPERSONIC EARTH ENTRY

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=392860 EFFECT OF NOSE-MOUNTED CONTROL-SYSTEM JETS IN ROLL-CONTROL POSITIONS ON THE AERODYNAMICS OF A SPACE VEHICLE ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=393145 By Suttles,John T. Nasa, Washington, D.C. 1966 . 26 , Bound With Nasa Tn D-3281-90

Place Hold on EFFECT OF NOSE-MOUNTED CONTROL-SYSTEM JETS IN ROLL-CONTROL POSITIONS ON THE AERODYNAMICS OF A SPACE VEHICLE

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=393145 A METHOD OF INTEGRAL RELATION SOLUTION FOR RADIATING,NONDIABATIC,INVISCID FLOW OVER A BLUNT BODY ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394073 By Suttles,John T.. Nasa, Washington, D.C. 1969 . 59 , Bound With Nasa Tn D-5471-80

Place Hold on A METHOD OF INTEGRAL RELATION SOLUTION FOR RADIATING,NONDIABATIC,INVISCID FLOW OVER A BLUNT BODY

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394073 A MODIFIED METHOD OF INTEGRAL RELATIONS APPROACH TO THE BLUNT-BODY EQULIBRIUM AIR FLOW FIELD,INCLUDIND COMPARISONS WITH INVERSE SOLUTIONS. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=398362 By Garrett,Bernard. Nasa, Washington, D.C. 1969 . 92 , Bound With Nasa Tn D-5421-5433,5435-5440.Lack No-5427.

Place Hold on A MODIFIED METHOD OF INTEGRAL RELATIONS APPROACH TO THE BLUNT-BODY EQULIBRIUM AIR FLOW FIELD,INCLUDIND COMPARISONS WITH INVERSE SOLUTIONS.

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=398362 AERODYNAMIC CHRACTERISTICS FROM MACH 0.22 TO 4.65 OF A TWO-STAGE ROCKET VEHICLE HAVING AN UNUSAL NOSE SHAPE. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=398517 By Suttles,John T. Nasa, Washington, D.C. 1964 . 59 , Bound With Nasa Tn D-2161-2162,2164-2170

Place Hold on AERODYNAMIC CHRACTERISTICS FROM MACH 0.22 TO 4.65 OF A TWO-STAGE ROCKET VEHICLE HAVING AN UNUSAL NOSE SHAPE.

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=398517 Aerodynamic characteristics from Mach 0.22 to 4.65 of a two-stage rocket vehicle having an unusual nose shape ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=564181 By Suttles, John T.. Washington, D.C. National Aeronautics and Space Administration [NASA] 1964 , Bound with NASA TN D-2162-2170

Place Hold on Aerodynamic characteristics from Mach 0.22 to 4.65 of a two-stage rocket vehicle having an unusual nose shape

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