Call Number (LC) Title Results
Y 3.N 21/5:6/578/2 Flight measurements of the dynamic longitudinal stability of several airplanes and a correlation of the measurements with pilots' observations of handling characteristics / 1
Y 3.N 21/5:6/579 Charts for calculating the performance of airplanes having constant-speed propellers /
Charts for calculating performance of airplanes having constant-speed propellers. 		3
Y 3.N 21/5:6/580 A general tank test of a model of the hull of the British Singapore IIC flying boat /
General tank test of model of hull of British Singapore IIC flying boat.
A General tank test of a model of the hull of the British Singapore IIC flying boat / 		3
Y 3.N 21/5:6/581 A study of autogiro rotor-blade oscillations in the plane of the rotor disk /
Study of autogiro rotor-blade oscillations in plane of rotor disk.
A Study of autogiro rotor-blade oscillations in the plane of the rotor disk / 		3
Y 3.N 21/5:6/582 Analysis and model tests of autogiro jump take-out /
Analysis and model tests of autogiro jump take-off.
Analysis and model tests of autogiro jump take-off / 		3
Y 3.N 21/5:6/583 Mixture distribution in a single-row radial engine /
Mixture distribution in single℗--row radial engine. 		3
Y 3.N 21/5:6/584 Effect of several factors on the cooling of a radial engine in flight /
Effect of several factors on cooling of radial engine in flight. 		3
Y 3.N 21/5:6/585 Mechanical properties of aluminum-alloy rivets /
Mechanical properties of aluminum-alloy rivets. 		3
Y 3.N 21/5:6/586 The reduction of aileron operating force by differential linkage /
Reduction of aileron operating force by differential linkage.
The Reduction of aileron operating force by differential linkage / 		3
Y 3.N 21/5:6/587 The forces and moments on airplane engine mounts /
Forces and moments on airplane engine mounts.
The Forces and moments on airplane engine mounts / 		3
Y 3.N 21/5:6/588 Strain measurements on small duralumin box beams in bending /
Strain measurements on small duralumin box beams in bending. 		3
Y 3.N 21/5:6/589 Theoretical span loading and moments of tapered wings produced by aileron deflection /
Theoretical span loading and moments of tapered wings produced by aileron deflection. 		3
Y 3.N 21/5:6/590 Hydrodynamic tests in the N.A.C.A. tank of a model of the hull of the short Calcutta flying boat /
Hydrodynamic tests in N. A. C. A. tank of model of hull of Short Calcutta flying boat. 		3
Y 3.N 21/5:6/591 Full-scale span load distribution on a tapered wing with split flaps of various spans /
Full-scale span load distribution on tapered wing with split flaps of various spans. 		3
Y 3.N 21/5:6/592 A study of the factors affecting the range of airplanes /
Study of factors affecting range of airplanes. 		3
Y 3.N 21/5:6/593 Pressure drop in tubing in aircraft instrument installations /
Pressure drop in tubing in aircraft instrument installations. 		3
Y 3.N 21/5:6/594 Tank tests of two models of flying-boat hulls to determine the effect of ventilating the step /
Tank tests of two models of flying-boat hulls to determine effect of ventilating the step. 		3
Y 3.N 21/5:6/595 Bending tests of circular cylinders of corrugated aluminum-alloy sheet /
Bending tests of circular cylinders of corrugated aluminum-alloy sheet. 		3
Y 3.N 21/5:6/596 Full-scale wind-tunnel and flight tests of a Fairchild 22 airplane equipped with a Zap flap and Zap ailerons /
Full-scale wind℗--tunnel and flight tests of Fairchild 22 airplane equipped with zap flap and zap ailerons. 		3
Y 3.N 21/5:6/597 Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps /
Notes on calculation of minimum horizontal tail surface for airplanes equipped with wing flaps. 		3