Call Number (LC) Title Results
Y 3.N 21/5:6/801 Tests of round and flat spoilers on a tapered wing in the NACA 19-foot pressure wind tunnel / 2
Y 3.N 21/5:6/802 Tests of a gust-alleviating wing in the gust tunnel / 2
Y 3.N 21/5:6/803 Some effects of rainfall on flight of airplanes and on instrument indications /
Some effects of rainfall on flight airplanes and on instrument indications / 		2
Y 3.N 21/5:6/804 Wind-tunnel investigation of the effect of vertical position of the wing on the side flow in the region of the vertical tail / 2
Y 3.N 21/5:6/805 Effect of aging on mechanical properties of aluminum-alloy rivets / 2
Y 3.N 21/5:6/806 Stresses and deflections in thin shells and curved plates due to concentrated and variously distributed loading / 2
Y 3.N 21/5:6/807 Spin tests of two models of a low-wing monoplane to investigate scale effect in the model test range / 2
Y 3.N 21/5:6/808 Wind-tunnel investigation of an NACA 23012 airfoil with several arrangements of slotted flaps with extended lips / 2
Y 3.N 21/5:6/809 The theoretical lateral motions of an automatically controlled airplane subjected to a yawing-moment disturbance /
The Theoretical lateral motions of an automatically controlled airplane subjected to a yawing-moment disturbance / 		2
Y 3.N 21/5:6/810 Preliminary stability and control tests in the NACA free-flight wind tunnel and correlation with full-scale flight tests / 2
Y 3.N 21/5:6/811 The effect of methods of testing on the ultimate loads supported by stiffened flat sheet panels under edge compression /
The Effect of methods of testing on the ultimate loads supported by stiffened flat sheet panels under edge compression / 		2
Y 3.N 21/5:6/812 Minimum induced drag in wing-fuselage interference / 2
Y 3.N 21/5:6/813 Cooling tests of an airplane equipped with an NACA cowling and a wing-duct cooling system / 2
Y 3.N 21/5:6/814 Effect of some present-day airplane design trends on requirements for lateral stability / 2
Y 3.N 21/5:6/815 Comparison of vee-type and conventional tail surfaces in combination with fuselage and wing in the variable-density tunnel / 2
Y 3.N 21/5:6/816 Cooling and performance tests of a Continental A-75 engine / 2
Y 3.N 21/5:6/817 Correction of the lifting-line theory for the effect of the chord / 2
Y 3.N 21/5:6/818 The tensile elastic properties at low temperatures of 18 : 8 Cr-Ni steel as affected by heat treatment and slight plastic deformation /
The Tensile elastic properties at low temperatures of 18:8 Cr-Ni steel as affected by heat treatment and slight plastic deformation / 		2
Y 3.N 21/5:6/819 Comparison of stress-strain curves obtained by single-thickness and pack methods / 2
Y 3.N 21/5:6/820 The aerodynamics of a wind-tunnel fan /
The Aerodynamics of a wind-tunnel fan / 		2