PKK Library Search for 'su:{Aircraft Design, Testing and Performance}'

NASA Technical Note [NASA TN D-443]: Preliminary investigation of a paraglider

Washington NASA 1960 . 25p , Bound together NASA TN D-441 to 450 | Bound vol. Acc. No. 63667 contains Acc. No. TR10185 to TR10193

Place Hold on NASA Technical Note [NASA TN D-443]: Preliminary investigation of a paraglider

NASA Technical Note [NASA TN D-448]: Some landing studies pertinent to glider-reentry vehicles

Washington NASA 1960 . 22p , Bound together NASA TN D-441 to 450 | Bound vol. Acc. No. 63667 contains Acc. No. TR10185 to TR10193

Place Hold on NASA Technical Note [NASA TN D-448]: Some landing studies pertinent to glider-reentry vehicles

NASA Technical Note [NASA TN D-544]: Measured base pressures on several twin rocket-nozzle configurations at mach numbers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins

Washington NASA 1960 . 19p , Bound together NASA TN D-541 to 550 | Bound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862

Place Hold on NASA Technical Note [NASA TN D-544]: Measured base pressures on several twin rocket-nozzle configurations at mach numbers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins

NASA Technical Note [NASA TN D-550]: Heat-transfer measurements on the apexes of two 60 [degree] sweptback delta wings (panel semiapex angle of 30 [degree]) having 0 [degree] and 45 [degree] dihedral at a mach number of 4.95

Washington NASA 1961 . 51p , Bound together NASA TN D-541 to 550 | Bound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862

Place Hold on NASA Technical Note [NASA TN D-550]: Heat-transfer measurements on the apexes of two 60 [degree] sweptback delta wings (panel semiapex angle of 30 [degree]) having 0 [degree] and 45 [degree] dihedral at a mach number of 4.95

NASA Technical Note [NASA TN D-382]: Effect of blade cutout on power required by helicopters operating at high tip-speed ratios

Washington NASA 1960 . 18p , Bound together NASA TN D-381 to 390 | Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611

Place Hold on NASA Technical Note [NASA TN D-382]: Effect of blade cutout on power required by helicopters operating at high tip-speed ratios

Airspeed operating practices of turbine-powered commercial transport airplanes

By Coleman, Martin R.. Washigton D. C. NASA 1961 . 26p. , Bound With NASA TN D-741-750

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NASA Technical Note [NASA TN D-541]: Landing-impact characteristics of load-alleviating struts on a model of a winged space vehicle

Washington NASA 1960 . 19p , Bound together NASA TN D-541 to 550 | Bound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862

Place Hold on NASA Technical Note [NASA TN D-541]: Landing-impact characteristics of load-alleviating struts on a model of a winged space vehicle