Call Number (LC) Title Results
Y 3.N 21/5:6/223 Determination of the lift and drag characteristics of an airplane in flight / 1
Y 3.N 21/5:6/224 Pressure distribution on the nose of an airship in circling flight / 1
Y 3.N 21/5:6/225 Propeller scale effect and body interference / 1
Y 3.N 21/5:6/226 Wind tunnel tests of fuselages and windshields / 2
Y 3.N 21/5:6/227 Determination and classification of the aerodynamic properties of wing sections / 1
Y 3.N 21/5:6/228 The Flettner rotor ship in the light of the Kutta-Joukowski theory and of experimental results / 1
Y 3.N 21/5:6/229 An altitude chamber for the study and calibration of aeronautical instruments / 1
Y 3.N 21/5:6/230 The spacing of orifices for the measurement of pressure distributions / 1
Y 3.N 21/5:6/231 The resistance to the steady motion of small spheres in fluids / 1
Y 3.N 21/5:6/232 The lateral failure of spars / 1
Y 3.N 21/5:6/233 N.A.C.A. flight-path-angle and air-speed recorder / 1
Y 3.N 21/5:6/234 An investigation of the characteristics of steel diaphragms for automatic fuel-injection valves / 1
Y 3.N 21/5:6/235 Propeller design practical application of the blade element theory - 1 /
Propeller design. 		2
Y 3.N 21/5:6/236 Extension of test data on a family of model propellers by means of the modified blade element theory - 2 /
Propeller design. 		2
Y 3.N 21/5:6/237 Propeller design. 1
Y 3.N 21/5:6/238 Propeller design.
Propeller design A simple method for determining the strength of propellers - 4 / 		2
Y 3.N 21/5:6/239 Steam power plants in aircraft / 1
Y 3.N 21/5:6/240 The N.A.C.A. CYH airfoil section / 2
Y 3.N 21/5:6/241 Tests of several bearing materials lubricated by gasoline / 1
Y 3.N 21/5:6/242 Improving the performance of a compression ignition engine by directing flow of the inlet air / 1