Call Number (LC) Title Results
Y 3.N 21/5:11/L530 Wind-tunnel tests of two Hamilton Standard propellers embodying Clark Y and NACA 16 series blade sections / 1
Y 3.N 21/5:11/L531 Tests of a 1/7-scale powered model of the Kaiser tailless airplane in the Langley full-scale tunnel / 1
Y 3.N 21/5:11/L532 A flight investigation of the boundary-layer characteristics and profile drag of the NACA 35-215 laminar-flow airfoil at high Reynolds numbers / 1
Y 3.N 21/5:11/L533 Wind-tunnel investigation of alternative propellers operating behind deflected wing flaps for the XB-36 airplane / 1
Y 3.N 21/5:11/L534 Investigation of surface irregularities on an NACA 63(420)-416, a = 1.0 airfoil section for the Glenn L. Martin Company design 195 / 1
Y 3.N 21/5:11/L535 Analysis of heat and compressibility effects in internal flow systems and high-speed tests of a ram-jet system / 1
Y 3.N 21/5:11/L536 The analysis of strains indicated by multiple-strand resistance-type wire strain gages used as rosettes / 1
Y 3.N 21/5:11/L537 Performance selection charts for gliders and twin-engine tow planes / 1
Y 3.N 21/5:11/L538 Longitudinal-trim tests of a 0.059-scale model of the Curtiss-Wright XP-55 airplane / 1
Y 3.N 21/5:11/L539 Tests of a 1/17-scale model of the XBDR-1 airplane in the NACA gust tunnel / 1
Y 3.N 21/5:11/L54 Experimental determination of the effect of negative dihedral on lateral stability and control characteristics at high lift coefficients / 1
Y 3.N 21/5:11/L540 Acceleration, stress, and deflection measurements on the XB-15 bomber in gusty air / 1
Y 3.N 21/5:11/L541 Estimation of the performance and longitudinal stability and control of a lifting-body type of cargo airplane from tests of simplified models / 1
Y 3.N 21/5:11/L542 High-speed drag tests of several fuselage shapes in combination with a wing / 1
Y 3.N 21/5:11/L543 Power-off wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane / 1
Y 3.N 21/5:11/L544 Aerodynamic data for a wing section of the Republic XF-12 airplane equipped with a double slotted flap / 1
Y 3.N 21/5:11/L545 Full-scale-tunnel performance tests of the PV-2 helicopter rotor / 1
Y 3.N 21/5:11/L546 The effect of altitude on bomber performance / 1
Y 3.N 21/5:11/L547 Flight measurements of the rudder control and sideslip characteristics of four vertical tail arrangements on the P-40 series airplanes / 1
Y 3.N 21/5:11/L548 Tail-load measurements on the XB-15 bomber in gusty air / 1