Call Number (LC) Title Results
Y 3.N 21/5:8/821 On the actual loads on airplane landing gears /
On the actual loads on airplane landing gears. 		2
Y 3.N 21/5:8/822 Turbulent boundary layer of an airfoil /
Turbulent boundary layer of an airfoil. 		2
Y 3.N 21/5:8/823 Experimental investigation of the problem of surface roughness /
Experimental investigation of the problem of surface roughness. 		2
Y 3.N 21/5:8/824 The photoelastic investigation of three-dimensional stress and strain conditions /
The photoelastic investigation of three-dimensional stress and strain conditions. 		2
Y 3.N 21/5:8/825 The source of propeller noise /
The source of propeller noise. 		2
Y 3.N 21/5:8/826 The scale effect in towing tests with airplane-float systems /
The scale effect in towing tests with airplane-float systems. 		2
Y 3.N 21/5:8/827 Helicopter problems /
Helicopter problems. 		2
Y 3.N 21/5:8/828 Ground effect - theory and practice /
Ground effect--theory and practice. 		2
Y 3.N 21/5:8/829 Method of curved models and its application to the study of curvilinear flight of airships. : Part 1 /
Method of curved models and its application to the study of curvilinear flight of airships, pt. 1. 		2
Y 3.N 21/5:8/830 Method of curved models and its application to the study of curvilinear flight of airships. : Part 2 /
Method of curved models and its application to the study of curvilinear flight of airships, pt. 2. 		2
Y 3.N 21/5:8/831 Contributions to the theory of incomplete tension bay /
Contributions to the theory of incomplete tension bay. 		2
Y 3.N 21/5:8/832 The critical velocity of a body towed by a cable from an airplane /
The critical velocity of a body towed by a cable from an airplane. 		2
Y 3.N 21/5:8/833 The apparent width of the plate in compression /
The apparent width of the plate in compression. 		2
Y 3.N 21/5:8/834 The stability of orthotropic elliptic cylinders in pure bending /
The stability of orthotropic elliptic cylinders in pure bending. 		2
Y 3.N 21/5:8/835 Pressure distribution on a wing section with slotted flap in free flight tests /
Pressure distribution on a wing section with slotted flap in free flight tests. 		2
Y 3.N 21/5:8/836 The ground effect on lifting propellers /
The ground effect on lifting propellers. 		2
Y 3.N 21/5:8/837 Charts for checking the stability of plane systems of rods /
Charts for checking the stability of plane systems of rods. 		2
Y 3.N 21/5:8/838 The strength of shell bodies - theory and practice /
The strength of shell bodies--theory and practice.
The strength of shell bodies-- theory and practice / 		3
Y 3.N 21/5:8/839 The design of airplane-engine superchargers.
The design of airplane-engine superchargers / 		2
Y 3.N 21/5:8/840 Research and design problems introduced by increased power output /
Research and design problems introduced by increased power output. 		2