Call Number (LC) | Title | Results |
---|---|---|
Y 3.N 21/5:8/913 |
Measurement of true dynamic and static pressures in flight. Measurement of the true dynamic and static pressures in flight / |
2 |
Y 3.N 21/5:8/914 |
Engine knock and combustion chamber form. Engine knock and combustion chamber form / |
2 |
Y 3.N 21/5:8/915 |
Experimental and analytical investigation of a monocoque wing model loaded in bending. Experimental and analytical investigation of monocoque wing model loaded in bending. |
2 |
Y 3.N 21/5:8/916 |
Activation of hydrocarbons and the octane number / Activation of hydrocarbons and octane number. |
2 |
Y 3.N 21/5:8/917 |
The effect of compressibility on the pressure reading of a Prandtl pitot tube at subsonic flow velocity / Effect of compressibility on pressure reading of Prandtl pitot tube at subsonic flow velocity. |
2 |
Y 3.N 21/5:8/918 |
The enlarged N.A.C.A. tank, and some of its work / Enlarged N. A. C. A. tank, and some of its work. |
2 |
Y 3.N 21/5:8/919 |
Report on ice formation on aircraft / Report on ice formation on aircraft. |
2 |
Y 3.N 21/5:8/920 |
The effect of the slipstream on an airplane wing / Effect of slipstream on airplane wing. |
2 |
Y 3.N 21/5:8/921 |
Contribution to the aerodynamics of rotating-wing aircraft / Contribution to aerodynamics of rotating-wing aircraft. |
2 |
Y 3.N 21/5:8/922 |
Breda wind tunnel. The Breda wind tunnel / |
2 |
Y 3.N 21/5:8/923 |
Measurement of the air-flow velocity in the cylinder of an airplane engine / Measurement of the air-flow velocity in the cylinder of an airplane engine. |
2 |
Y 3.N 21/5:8/924 |
Modern methods of fuel testing / Modern methods of fuel testing. |
2 |
Y 3.N 21/5:8/925 |
Effect of wing loading, aspect ratio, and span loading of flight performances / Effect of Wing Loading, Aspect Ratio, and Span Loading on Flight Performances. |
2 |
Y 3.N 21/5:8/926 |
DFS dive-control brakes for gliders and airplanes. : and Analytical study of the drag of the DFS dive-control brake / DFS Dive-Control Brakes for Gliders and Airplanes. |
2 |
Y 3.N 21/5:8/927 |
Constant-pressure blowers / Constant-Pressure Blowers. |
2 |
Y 3.N 21/5:8/928 |
Knocking in an internal-combustion engine / Knocking in an Internal-Combustion Engine. |
2 |
Y 3.N 21/5:8/929 |
Aerodynamics of Rotating-Wing Aircraft with Blade-Pitch Control. Aerodynamics of rotating-wing aircraft with blade-pitch control / |
2 |
Y 3.N 21/5:8/930 |
Experimental Contribution to the Study of Combustion in Compression-Ignition Engines. Experimental contribution to the study of combustion in compression-ignition engines / |
2 |
Y 3.N 21/5:8/931 |
Testing of high-octane fuels in the single-cylinder airplane engine / Testing of High-Octane Fuels in the Single-Cylinder Airplane Engine. |
2 |
Y 3.N 21/5:8/932 |
Theoretical and experimental investigations of the drag of installed aircraft radiators / Theoretical and Experimental Investigations of the Drag of Installed Aircraft Radiators. |
2 |