<![CDATA[PKK Library Search for 'au:"Carlson,Harry W"']]>

<![CDATA[PKK Library Search for 'au:"Carlson,Harry W"']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Carlson%2CHarry%20W%22&format=rss2 12 0 200 APPLICATION OF SONIC-BOOM MINIMIZATION CONCEPTS IN SUPERSONIC TRANSPORT DESIGN ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394490 By Carlson,Harry W, Barger,Raymond L. Nasa, Washington, D.C. 1973 . 57 , Bound With Nasa Tn D-7211-19

Place Hold on APPLICATION OF SONIC-BOOM MINIMIZATION CONCEPTS IN SUPERSONIC TRANSPORT DESIGN

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394490 THE SHOCK-WAVE NOISE PROBLEM OF SUPERSONIC AIRCRAFT IN STEADY FLIGHT ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=395610 By Maglieri,Domenic J. Nasa, Washington, D.C. 1959 . 15 , Bound With Tr007387-88, Tr007390-98

Place Hold on THE SHOCK-WAVE NOISE PROBLEM OF SUPERSONIC AIRCRAFT IN STEADY FLIGHT

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=395610 CORRELATION OF SONIC-BOOM THEORY WITH WIND-TUNNEL AND FLIGHT MEASUREMENTS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=397299 By Carlson,Harry W. Nasa, Washington, D.C. 1964 . 25 , Bound With Nasa Tr R-211-12,214-20

Place Hold on CORRELATION OF SONIC-BOOM THEORY WITH WIND-TUNNEL AND FLIGHT MEASUREMENTS

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=397299 SONIC-BOOM CHRACTERISTICS IN THE EXTERME NEAR FIELS OF A COMPLEX AIRPLANE MODEL AT MACH NUMBERS OF 1.5,1.8 AND 2.5. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=398700 By Morris,Odell A,Lamb,Milton. Nasa, Washington, D.C. 1970 . 26 , Bound With Nasa Tn D-5751-5754,5756-5759.

Place Hold on SONIC-BOOM CHRACTERISTICS IN THE EXTERME NEAR FIELS OF A COMPLEX AIRPLANE MODEL AT MACH NUMBERS OF 1.5,1.8 AND 2.5.

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=398700 PRESSURE DISTRIBUTIONS AT MACH NUMBER 2.05 ON A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=399129 By Carlson,Harry W. Nasa, Washington, D.C. 1962 . 40 , Bound With Nasa Tn D-1261-1263,1265-1270

Place Hold on PRESSURE DISTRIBUTIONS AT MACH NUMBER 2.05 ON A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=399129 A STUDY OF THE APPLICATION OF HEAT OR FORCE FIELDS TO THE SONIC-BOOM -MINIMIZATION PROBLEM ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=400128 By Miller,David S. Nasa, Washington, D.C. 1969 . 17 , Bound With Nasa Tn D-5580-5581,5583-5589

Place Hold on A STUDY OF THE APPLICATION OF HEAT OR FORCE FIELDS TO THE SONIC-BOOM -MINIMIZATION PROBLEM

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=400128 AERODYNAMIC CHARACTERISTICS AT MACH NUMBER 2.05 OF A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=401277 By Carlson,Harry W. Nasa, Washington, D.C. 1960 . 34 , Bound Wind Nasa Tm X-300-17,334-45 Lack No.301-04,306-12,315-16,318-31,333,335,337,339-43

Place Hold on AERODYNAMIC CHARACTERISTICS AT MACH NUMBER 2.05 OF A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=401277 Amodification to linearized theory for prediction of pressure loagings on lifting surfaces at high supersonic mach numbers and large angles of attack ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=404692 By Carlson, Harry W..

Place Hold on Amodification to linearized theory for prediction of pressure loagings on lifting surfaces at high supersonic mach numbers and large angles of attack

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=404692 A NUMERICAL METHOD FOR CALCULATING THE FLAT-PLATE PRESSURE DISTRIBUTIONS ON SUPERSONIC WINGS OF ARBITRARY PLANFORM ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=479557 By MIDDLETON,WILBUR D. NASA, WASHINGTON, D.C. 1965 . ,23,,,,,, , Bound with NASA TN D-2571-2569

Place Hold on A NUMERICAL METHOD FOR CALCULATING THE FLAT-PLATE PRESSURE DISTRIBUTIONS ON SUPERSONIC WINGS OF ARBITRARY PLANFORM

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=479557 A NUMERICAL METHOD FOR THE DESIGN OF CAMBER SURFACES OF SUPERSONIC WINGS WITH ARBITRARY PLANFORMS. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=479600 By CARLSON,HARRY W. NASA, WASHINGTON, D.C. 1964 . ,18,,,,,, , Bound with NASA TN D-2342-50.

Place Hold on A NUMERICAL METHOD FOR THE DESIGN OF CAMBER SURFACES OF SUPERSONIC WINGS WITH ARBITRARY PLANFORMS.

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=479600 A numerical method for calculating the flat-plate pressure distribution on supersonic wings of supersonic wings of arbitrary planform. [NASA TN D-2570] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=563321 By Wilbur, D. Middleton. Washington, D. C NASA 1965 . 23p

Place Hold on A numerical method for calculating the flat-plate pressure distribution on supersonic wings of supersonic wings of arbitrary planform. [NASA TN D-2570]

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=563321 Sonic boom characteristics of proposed supersonic and hypersonic airplanes [NASA TN D-3587] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=564389 By McLean, F. Edward. Washington,D.C. National Aeronautics and Space Administration . 15p

Place Hold on Sonic boom characteristics of proposed supersonic and hypersonic airplanes [NASA TN D-3587]

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