Call Number (LC) Title Results
Y 3.N 21/5:6/565 Influence of fuel-oil temperature on the combustion in a prechamber compression-ignition engine /
Influence of fuel-oil temperature on combustion in pre-chamber compression-ignition engine. 		3
Y 3.N 21/5:6/566 Tank tests of a model of the NC flying-boat hull - N.A.C.A. Model 44 /
Tank tests of model of NC flying-boat hull, N. A. C. A. model 44. 		3
Y 3.N 21/5:6/567 Tests of N.A.C.A. airfoils in the variable-density wind tunnel.
Tests of N. A. C. A. airfoils in variable-density wind tunnel, series 230.
Tests of N.A.C.A. airfoils in the variable-density wind tunnel. : Series 230 / 		3
Y 3.N 21/5:6/568 Calculated effect of various types of flap on take-off over obstacles /
Calculated effect of various types of flap on take-off over obstacles. 		3
Y 3.N 21/5:6/569 Boosted performance of a compression-ignition engine with a displacer piston /
Boosted performance of compression-ignition engine with a displacer piston. 		3
Y 3.N 21/5:6/570 Effect of changes in tail arrangement upon the spinning of a low-wing monoplane model /
Effect of changes in tail arrangement upon spinning of low-wing monoplane model. 		3
Y 3.N 21/5:6/571 A method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y /
A Method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y /
Method of estimating aerodynamic effects of ordinary and split flaps of airfoils. 		3
Y 3.N 21/5:6/572 Performance of air-cooled engine cylinders using blower cooling /
Performance of air℗--cooled engine cylinders using blower cooling. 		3
Y 3.N 21/5:6/573 Carbon-monoxide indicators for aircraft /
Carbon-monoxide indicators for aircraft. 		2
Y 3.N 21/5:6/574 Tank tests of models of flying boat hulls having longitudinal steps /
Tank tests of models of flying boat hulls having longitudinal steps. 		3
Y 3.N 21/5:6/575 Estimation of moments of inertia of airplanes from design data /
Estimation of moments of inertia of airplanes from design data. 		3
Y 3.N 21/5:6/576 Tank tests of a model of the hull of the Navy PB-1 flying boat - N.A.C.A. Model 52 /
Tank tests of model of hull of Navy PB-1 flying boat, N. A. C. A. model 52. 		3
Y 3.N 21/5:6/577 Friction of compression-ignition engines /
Friction of compression-ignition engines. 		3
Y 3.N 21/5:6/578 Full-scale wind-tunnel and flight tests of a Fairchild 22 airplane equipped with a Fowler flap /
Full℗--scale wind℗--tunnel and flight tests of Fairchild 22 airplane equipped with Fowler flap. 		3
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 /
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. 		3
Y 3.N 21/5:6/581 A Study of autogiro rotor-blade oscillations in the plane of the rotor disk /
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. 		3
Y 3.N 21/5:6/582 Analysis and model tests of autogiro jump take-off /
Analysis and model tests of autogiro jump take-out /
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