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Y 3.N 21/5:11/L310
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Comparison of an approximate and an exact method of shear-lag analysis / |
1 |
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Y 3.N 21/5:11/L311
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Wind-tunnel tests of two tapered wings with straight leading edges and with constant-chord center secitons of different spans / |
1 |
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Y 3.N 21/5:11/L312
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Theory of mechanical oscillations of rotors with two hinged blades / |
1 |
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Y 3.N 21/5:11/L313
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On the plane potential flow past a lattice of arbitrary airfoils / |
1 |
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Y 3.N 21/5:11/L314
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Wind-tunnel investigation of control-surface characteristics. : 13 - Various flap overhangs used with a 30-percent-chord flap on an NACA 66-009 airfoil / |
1 |
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Y 3.N 21/5:11/L315
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Effect of countersunk depth on the tightness of two types of machine-countersunk rivet / |
1 |
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Y 3.N 21/5:11/L316
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Wind-tunnel tests of single- and dual-rotating tractor propellers at low blade angles and of two- and three-blade tractor propellers at blade angles up to 65 degrees / |
1 |
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Y 3.N 21/5:11/L317
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Wind-tunnel investigation of plain ailerons for a wing with a full-span flap consisting of an inboard Fowler and an outboard retractable split flap / |
1 |
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Y 3.N 21/5:11/L318
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Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons / |
1 |
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Y 3.N 21/5:11/L319
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Formulas for use in boundary-layer calculations on low-drag wings / |
1 |
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Y 3.N 21/5:11/L32
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Column and plate compressive strengths of aircraft structural materials. : Extruded 24S-T aluminum-alloy / |
1 |
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Y 3.N 21/5:11/L320
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The flow of a compressible fluid past a curved surface / |
1 |
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Y 3.N 21/5:11/L321
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The design of cooling ducts with special reference to the boundary layer at the inlet / |
1 |
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Y 3.N 21/5:11/L322
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Analysis of wind-tunnel stability and control tests in terms of flying qualities of full-scale airplanes / |
1 |
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Y 3.N 21/5:11/L323
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The strength and stiffness of shear webs with round lightening holes having 45 degree flanges / |
2 |
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Y 3.N 21/5:11/l324
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An approximate method of shear-lag analysis for beams loaded at right angles to the plane of symmetry of the cross section / |
1 |
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Y 3.N 21/5:11/L325
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Wind-tunnel tests of ailerons at various speeds. : 3 - Ailerons of 0.20 airfoil chord and true contour with 0.35-aileron-chord Frise balance on the NACA 23012 airfoil / |
1 |
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Y 3.N 21/5:11/L326
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Principles of moment distribution applied to stability of structures composed of bars or plates / |
1 |
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Y 3.N 21/5:11/L327
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Wind-tunnel vibration tests of a four-blade single-rotating pusher propeller / |
1 |
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Y 3.N 21/5:11/L328
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Investigation of air flow in right-angle elbows in a rectangular duct / |
1 |
