Call Number (LC) Title Results
Y 3.N 21/5:8/1038 The performance of a vaneless diffuser fan /
The Performance of a Vaneness Diffuser Fan. 		2
Y 3.N 21/5:8/1039 Pressure distribution in nonuniform two-dimensional flow /
Pressure Distribution in Nonuniform Two-Dimensional Flow. 		2
Y 3.N 21/5:8/1040 Piezoelectric instruments of high natural frequency vibration characteristics and protection against interferenece by mass forces /
Piezoelectric Instruments of High Natural frequency Vibration Characteristics and Protection Against Interference by Mass Forces. 		2
Y 3.N 21/5:8/1041 Tail Buffeting.
Tail buffeting / 		2
Y 3.N 21/5:8/1042 Theoretical Determination of Axial Fan Performance.
Theoretical determination of axial fan performance / 		2
Y 3.N 21/5:8/1043 Experimental investigation of a model of a two-stage turboblower /
Experimental Investigation of a Model of a Two-Stage Turnblower. 		2
Y 3.N 21/5:8/1044 Heat Transfer of Airfoils and Plates.
Heat transfer of airfoils and plates / 		2
Y 3.N 21/5:8/1045 The heat transfer to a plate in flow at high speed /
The Heat Transfer to a Plate in Flow at High Speed. 		2
Y 3.N 21/5:8/1046 Experimental investigation of impact in landing on water /
Experimental Investigation of Impact in Landing on Water. 		2
Y 3.N 21/5:8/1047 Heat transfer through turbulent friction layers /
Heat Transfer Through Turbulent Friction Layers. 		2
Y 3.N 21/5:8/1048 Periodic heat transfer at small pressure fluctations /
Periodic Heat Transfer at Small Pressure Fluctuations. 		2
Y 3.N 21/5:8/1049 Researches on preliminary chemical reactions in spark-ignition engines /
Researches on Preliminary Chemical Reactions in Spark-Ignition Engines. 		2
Y 3.N 21/5:8/1050 Heat transfer over the circumference of a heated cylinder in transverse flow /
Heat Transfer Over the Circumference of a Heated Cylinder in Transverse Flow. 		2
Y 3.N 21/5:8/1051 The coupling of flexural propeller vibrations with the torsional crankshaft vibrations /
The Coupling of Flexual Propeller Vibrations with the Torsional Crankshaft Vibrations. 		2
Y 3.N 21/5:8/1052 Determination of the Mass Moments and Radii of Inertia of the Sections of a Tapered Wing and the Center-of-Gravity Line Along the Wing Span.
Determination of the mass moments and radii of inertia of the sections of a tapered wing and the center-of-gravity line along the wing span / 		2
Y 3.N 21/5:8/1053 Turbulent friction in the boundary layer of a flat plate in a two-dimensional compressible flow at high speeds /
Turbulent Friction in the Boundary Layer of a Flat Plate in a Two-Dimensional Compressible Flow at High Speeds. 		2
Y 3.N 21/5:8/1054 Heat transfer and hydraulic flow resistance for streams of high velocity /
Heat Transfer and Hydraulic Flow Resistance for Streaks of High Velocity. 		2
Y 3.N 21/5:8/1055 Determination of the stresses produced by the landing impact in the bulkheads of a seaplane bottom /
Determination of the Stresses Produced by the Landing Impact in the Bulkhead of a Seaplane Bottom. 		2
Y 3.N 21/5:8/1056 Piston ring pressure distribution / 1
Y 3.N 21/5:8/1057 Researches on the piston ring /
Researches on the Piston Ring. 		2