Call Number (LC) Title Results
Y 3.N 21/5:5/793 Experiments on drag of revolving disks, cylinders, and streamline rods at high speeds. 1
Y 3.N 21/5:5/794 The flow of a compressible fluid past a circular arc profile. 1
Y 3.N 21/5:5/795 The NACA impact basin and water landing tests of a float model at various velocities and weights. 1
Y 3.N 21/5:5/798 Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers. 1
Y 3.N 21/5:5/800 Effects of small angles of sweep and moderate amounts of dihedral on stalling and lateral characteristics of a wing-fuselage combination equipped with partial- and full-span double slotted flaps. 1
Y 3.N 21/5:5/801 A method for studying the hunting oscillations of an airplane with a simple type of automatic control. 1
Y 3.N 21/5:5/803 Wind-tunnel investigation of the effects of profile modification and tabs on the characteristics of ailerons on a low-drag airfoil. 1
Y 3.N 21/5:5/805 An analysis of life expectancy of airplane wings in normal cruising flight. 1
Y 3.N 21/5:5/887 Critical-stress of thin-walled cylinders in axial compression / 1
Y 3.N 21/5:5/934 Recommendations for numerical solution of reinforced-panel and fuselage-ring problems / 1
Y 3.N 21/5:5/1135 Equations, tables, and charts for compressible flow. 1
Y 3.N 21/5:6/ A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory / 1
Y 3.N 21/5:6/1 Notes on longitudinal stability and balance / 1
Y 3.N 21/5:6/2 Airplane performance as influenced by the use of a supercharged engine / 1
Y 3.N 21/5:6/3 Notes on the theory of the accelerometer / 1
Y 3.N 21/5:6/4 The problem of the helicopter / 1
Y 3.N 21/5:6/5 Relation of rib spacing to stress in wing planes / 1
Y 3.N 21/5:6/6 Static testing and proposed standard specifications / 1
Y 3.N 21/5:6/7 Notes on the design of supercharged and over-dimensioned aircraft engines / 1
Y 3.N 21/5:6/8 Duralumin / 1