| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:6/1029 |
A condition on the initial shock / A condition on the initial shock. |
2 |
| Y 3.N 21/5:6/1030 |
The fatigue characteristics of bolted lap joints of 24S-T Alclad sheet materials. The Fatigue characteristics of bolted lap joints of 24S-T alclad sheet materials / |
2 |
| Y 3.N 21/5:6/1031 |
A Multiple bridge for elimination of contact-resistance errors in resistance strain-gage measurements / A multiple bridge for elimination of contact-resistance errors in resistance strain-gage measurements. |
2 |
| Y 3.N 21/5:6/1032 |
Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound / Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound. |
2 |
| Y 3.N 21/5:6/1033 |
Wing plan forms for high-speed flight / Wing plan forms for high-speed flight. |
2 |
| Y 3.N 21/5:6/1034 |
Bending-torsion flutter calculations modified by subsonic compressibility corrections / Bending-torsion flutter calculations modified by subsonic compressibility corrections. |
2 |
| Y 3.N 21/5:6/1035 |
Steady- and intermittent-flow coefficients of poppet intake valves / Steady- and intermittent-flow coefficients of poppet intake valves. |
2 |
| Y 3.N 21/5:6/1036 |
Comparison of static strengths of machine countersunk riveted joints in 24S-T, X75S-T, and Alclad 75S-T sheet / Comparison of static strengths of machine countersunk riveted joints in 24S-T, X75S-T, and Alclad 75S-T sheet. |
2 |
| Y 3.N 21/5:6/1037 |
A Study of combustion in a flowing gas / A study of combustion in a flowing gas. |
2 |
| Y 3.N 21/5:6/1038 |
Structural hinge-moment increments caused by hinge-axis distortion / Structural hinge-moment increments caused by hinge-axis distortion. |
2 |
| Y 3.N 21/5:6/1039 |
Quantitative treatment of the creep of metals by dislocation and rate-process theories / Quantitative treatment of the creep of metals by dislocation and rate-process theories. |
2 |
| Y 3.N 21/5:6/1040 |
Wake studies of eight models propellers / Wake studies of eight model propellers. |
2 |
| Y 3.N 21/5:6/1041 |
Effect of normal pressure on strength of axially loaded sheet-stringer panels / Effect of normal pressure on strength of axially loaded sheet-stringer panels. |
2 |
| Y 3.N 21/5:6/1042 |
Performance tests of wire strain gages. : 4 - Axial and transverse sensitivities / Performance tests of wire strain gages, 4 - axial and transverse sensitivities. |
2 |
| Y 3.N 21/5:6/1043 |
Charts for the rapid calculation of the work required to compress dry air / Charts for the rapid calculation of the work required to compress dry air. |
2 |
| Y 3.N 21/5:6/1044 |
Effect of Mach and Reynolds numbers on maximum lift coefficients / Effect of Mach and Reynolds numbers of maximum lift coefficient. |
2 |
| Y 3.N 21/5:6/1045 |
Tail-design requirements for satisfactory spin recovery / Tail-design requirements for satisfactory spin recovery. |
2 |
| Y 3.N 21/5:6/1046 |
Preliminary wind-tunnel investigation at low speed of stability and control characteristics of swept-back wings. Preliminary wind-tunnel investigation at low speed of stability and control characteristics of swept-back wings / |
2 |
| Y 3.N 21/5:6/1047 | Clamped long rectangular plate under combined axial load and normal pressure. | 1 |
| Y 3.N 21/5:6/1048 |
Two-dimensional wind-tunnel investigation of low-drag vertical-tail, horizontal-tail, and wing sections equipped with sealed internally balanced control surfaces / Two-dimensional wind-tunnel investigation of low-drag vertical-tail, horizontal-tail, and wing sections equipped with sealed internally balanced control surfaces. |
2 |
