<![CDATA[PKK Library Search for 'au:"Lichtenstein,Jacob H"']]>

<![CDATA[PKK Library Search for 'au:"Lichtenstein,Jacob H"']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Lichtenstein%2CJacob%20H%22&format=rss2 5 0 200 SOME STATIC, OSCILLATORY, AND FREE-BODY TESTS OF BLUNT BODIES AT LOW SUBSONIC SPEEDS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=393776 By Lichtenstein,Jacob H. Nasa, Washington, D.C. 1959 . 30 , Bound With Nasa Memo 2-15-59l-2-28-59l

Place Hold on SOME STATIC, OSCILLATORY, AND FREE-BODY TESTS OF BLUNT BODIES AT LOW SUBSONIC SPEEDS

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=393776 NASA Technical Note [NASA TN D-6113]: A statistical study of ability of simulated pilots to control the approach and descent of the lunar module to the lunar surface ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=398522 Washington NASA 1971 . 57p , Bound together NASA TN D-6110 to 6118 | Bound vol. Acc. No. 101227 contains Acc. No. TR13899 to TR13906

Place Hold on NASA Technical Note [NASA TN D-6113]: A statistical study of ability of simulated pilots to control the approach and descent of the lunar module to the lunar surface

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=398522 A PRELIMINARY INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE ON THE ROLLING DERIVATIVES OF AN UNSWEPT-WING MODEL OSCILLATING IN ROLL ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=399525 By Fisher,Lewis R,Lichtenstein,Jacob H. Naca, Washington 1955 . 29 , Bound With Naca Tn 3550-3553,3555-3559

Place Hold on A PRELIMINARY INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE ON THE ROLLING DERIVATIVES OF AN UNSWEPT-WING MODEL OSCILLATING IN ROLL

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=399525 COMPUTED LATERAL POWER SPECTRAL DENSITY RESPONSE OF CONVENTIONAL AND STOL AIRPLANES TO RANDOM ATMOSPHERIC TURBULENCE ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=399819 By Lichtenstein,Jacob H. Nasa, Washington, D.C. 1974 . 88 , Bound With Nasa Tn D-7440-43,7445-48

Place Hold on COMPUTED LATERAL POWER SPECTRAL DENSITY RESPONSE OF CONVENTIONAL AND STOL AIRPLANES TO RANDOM ATMOSPHERIC TURBULENCE

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=399819 LOW-SPEED INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE OF OSCILLATION IN SIDESLIP ON THE LATERAL STABILITY DERIVATIVES OF A 60(DEGREE) DELTA WING, A 45(DEGRE) SWEPTBACK WING, AND AN - - - ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=401695 By Lichtenstein,Jacob H. Nasa, Washington, D.C. 1961 . 19 , Bound With Nasa Tn D-891-895,897-900

Place Hold on LOW-SPEED INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE OF OSCILLATION IN SIDESLIP ON THE LATERAL STABILITY DERIVATIVES OF A 60(DEGREE) DELTA WING, A 45(DEGRE) SWEPTBACK WING, AND AN - - -

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