<![CDATA[PKK Library Search for 'au:"Gainer,Thomas G"']]>

<![CDATA[PKK Library Search for 'au:"Gainer,Thomas G"']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Gainer%2CThomas%20G%22&format=rss2 5 0 200 LOW SPEED INVESTIGATION OF THE EFFECTS OF WING SWEEP ON THE AERODYNAMIC CHARACTERISTICS OF PARAWINGS HAVING EQUAL-LENGTH LEADING EDGES AND KEEL ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394382 By Naeseth,Rodger L. Nasa, Washington, D.C. 1963 . 78 , Bound With Nasa Tn D-1951-1960

Place Hold on LOW SPEED INVESTIGATION OF THE EFFECTS OF WING SWEEP ON THE AERODYNAMIC CHARACTERISTICS OF PARAWINGS HAVING EQUAL-LENGTH LEADING EDGES AND KEEL

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394382 SUMMARY OF TRANSFORMATION EQUATIONS AND EQUATIONS OF MOTION USED IN FREE-FLIGHT AND WIND-TUNNEL DATA REDUCTION AND ANALYSIS. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=395572 By Gainer,Thomas G. National Aeronautics And Space Administration, Washington, D.C. 1972 . 119 , Bound With Nasa Sp-3064-65,3072 Lack No3066-69,3071

Place Hold on SUMMARY OF TRANSFORMATION EQUATIONS AND EQUATIONS OF MOTION USED IN FREE-FLIGHT AND WIND-TUNNEL DATA REDUCTION AND ANALYSIS.

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=395572 ROLLING STABILITY DERIVATIVES OF A VARIABLE-SWEEP TACTICAL FIGHTER MODEL AT SUBSONIC AND TRANSONIC SPEEDS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=398784 By Henderson,William P,Phillips,W Pelham. Nasa, Washington, D.C. 1967 . 54 , Bound With Nasa Tn D-3841-3844,3846-3850

Place Hold on ROLLING STABILITY DERIVATIVES OF A VARIABLE-SWEEP TACTICAL FIGHTER MODEL AT SUBSONIC AND TRANSONIC SPEEDS

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=398784 LOW-SPEED WIND-TUNNEL INVESTIGATION TO DETERMINE THE AERODYNAMIC CHARACTERISTICS OF A RECTANGULAR WING EQUIPPED WITH A FULL-SPAN AND AN INBOARD HALF-SPAN JET-AUGMENTED FLAP DEFLECTED 55 DEGREE ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=400899 By Gainer,Thomas G. Nasa, Washington, D.C. 1959 . 21 , Bound With Nasa Memo 1-15-59l-26,30-31, Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l

Place Hold on LOW-SPEED WIND-TUNNEL INVESTIGATION TO DETERMINE THE AERODYNAMIC CHARACTERISTICS OF A RECTANGULAR WING EQUIPPED WITH A FULL-SPAN AND AN INBOARD HALF-SPAN JET-AUGMENTED FLAP DEFLECTED 55 DEGREE

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=400899 INVESTIGATION OF OPENING CHARACTERISTICS OF AN ALL FLEXIABLE PARAWING. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=483201 By GAINER,THOMAS G. NASA, WASHINGTON, D.C. 1969 . ,30,,,,,, , Bound with NASA TN D-5031,5033-5040.

Place Hold on INVESTIGATION OF OPENING CHARACTERISTICS OF AN ALL FLEXIABLE PARAWING.

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