PKK Library Search for 'au:"Saltzman,Edwin J"'

IN-FLIGHT USE OF TRAVERSING BOUNDARY-LAYER PROBES

By Saltzman, Edwin J.. , Bound With: Nasa Tn D-6403-28

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PRELIMINARY BASE PRESSURE OBTAINED FROM THE X-15 AIRPLANE AT MACH NUMBERS FROM 1.1 TO 3.2

By Saltzman,Edwin J. Nasa, Washington, D.C. 1961 . 28 , Bound With Nasa Tn D-1051-1060

Place Hold on PRELIMINARY BASE PRESSURE OBTAINED FROM THE X-15 AIRPLANE AT MACH NUMBERS FROM 1.1 TO 3.2

FLIGHT INVESTIGATION OF THE EFFECT OF DISTRIBUTION ROUGHNESS ON SKIN DRAG OF A FULL-SCALE AIRPLANE

By Saltzman,Edwin J. Nasa, Washington, D.C. 1959 . 27 , Bound With Nasa Tm X-22-39

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FLIGHT DEMONSTRATION OF A SKIN-FRICTION GAGE TO A LOCAL MACH NUMBER OF 4.9

By Garringer,Darwin J. Nasa, Washington, D.C. . 25 , Bound With Nasa Tn D-3821-29

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PRILIMINARY FULL-SCALE POWER-OFF DRAG OF THE X-15 AIRPLANE FOR MACH NUMBERS FROM 0.7 TO 3.1

By Saltzman,Edwin J. Nasa, Washington, D.C. 1961 . 23 , Bound With Nasa Tm X-416-27,431-79 Lack No.418-22,24,26,28-29,32,34-36,38,42-47,50-58,60-66,69-78

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SOME TURBULENT BOUNDARY-LAYER MEASUREMENTS OBTAINED FROM THE FOREBODY OF AN MACH NUMBERS UP TO 1.72.

By Saltzman,Edwin J. Nasa, Washington, D.C. 1970 . 45 , Bound With Nasa Tn D-5831-37, 5839-40

Place Hold on SOME TURBULENT BOUNDARY-LAYER MEASUREMENTS OBTAINED FROM THE FOREBODY OF AN MACH NUMBERS UP TO 1.72.

FLIGHT TECHNIQUES FOR DETERMINING AIRPLANE DRAG AT HIGH MACH NUMBERS

By Beeler,De E,Bellman,Donald R. North Atlantic Treaty Organization,Paris 1956 . 23 , Bound With Nato Agard 81-83,85-90

Place Hold on FLIGHT TECHNIQUES FOR DETERMINING AIRPLANE DRAG AT HIGH MACH NUMBERS

Local skin friction coefficients and boundary layer profiles obtained in flight from the XB-70-1 airplane at mach numbers up to 2.5 [ NASA TN D-7220 ]

By Fisher, David F.. Washington,D.C. National Aeronautics and Space Administration 1973 . 68p

Place Hold on Local skin friction coefficients and boundary layer profiles obtained in flight from the XB-70-1 airplane at mach numbers up to 2.5 [ NASA TN D-7220 ]