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

<![CDATA[PKK Library Search for 'au:"Winston, Matthew M."']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Winston%2C%20Matthew%20M.%22&format=rss2 5 0 200 WIND-TUNNEL INVESTIGATION OF STEADY-STATE AERODYNAMICS OF A COMPOSITE-LIFT VTOL AIRCRAFT MODEL [NASA TN D-5232] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=395158 By Winston, Matthew M.. Washington, D.C. National Aeronautics and Space Administration 1969 . 38p , Bound With Nasa Tn D-5231-40

Place Hold on WIND-TUNNEL INVESTIGATION OF STEADY-STATE AERODYNAMICS OF A COMPOSITE-LIFT VTOL AIRCRAFT MODEL [NASA TN D-5232]

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=395158 A HOVERING INVESTIGATION OF AN EXTREMELY FLEXIBLE LIFTING ROTOR ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=396835 By Winston,Matthew M. Nasa, Washington, D.C. 1968 . 52

Place Hold on A HOVERING INVESTIGATION OF AN EXTREMELY FLEXIBLE LIFTING ROTOR

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=396835 INDUCED INTERFERENCE EFFECTS ON THE AERODYNAMIC CHARACTERISTICS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=397506 By Winston,Matthew M. Nasa, Washington, D.C. 1970 . 73 , Bound With Nasa Tn D-5720-5726,5728-5729

Place Hold on INDUCED INTERFERENCE EFFECTS ON THE AERODYNAMIC CHARACTERISTICS

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=397506 DATA FROM A STATIC-THRUST INVESTIGATION OF A LARGE-SCALE GENERAL RESEARCH VTOL-STOL MODEL IN GROUND EFFECT ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=400473 By Huston,Robert J. Nasa, Washington, D.C. 1960 . 66 , Bound With Nasa Tn D-391-96,398-400

Place Hold on DATA FROM A STATIC-THRUST INVESTIGATION OF A LARGE-SCALE GENERAL RESEARCH VTOL-STOL MODEL IN GROUND EFFECT

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=400473 WING AND FLAP LOADS OBTAINED FROM A WIND-TUNNEL INVESTIGATION OF A LARGE-SCALE V/STOL MODEL ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=400693 By Huston,Robert J,Ward,John F. Nasa, Washington, D.C. 1963 . 89 , Bound With Nasa Tn D-1631-33,1635-40

Place Hold on WING AND FLAP LOADS OBTAINED FROM A WIND-TUNNEL INVESTIGATION OF A LARGE-SCALE V/STOL MODEL

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