NAS 1.60:1281
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Effect of concentration dependence of the diffusion coefficient on homogenization kinetics in multiphase binary alloy systems / |
1 |
NAS 1.60:1282
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An alternating direction implicit method for the control data STAR-100 vector computer / |
1 |
NAS 1.60:1283
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Effect of vibration duration on human discomfort / |
1 |
NAS 1.60:1284
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Reinforced carbon-carbon oxidation behavior in convective and radiative environments / |
1 |
NAS 1.60:1285
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Development and validation of a piloted simulation of a helicopter and external sling load / |
1 |
NAS 1.60:1286
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A decoding procedure for the Reed-Solomon codes / |
1 |
NAS 1.60:1287
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Effect of geometry on hydrodynamic film thickness / |
1 |
NAS 1.60:1288
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Microstructure and mechanical properties of quenched and tempered 300M steel / |
1 |
NAS 1.60:1290
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Effects of spanwise blowing on the surface pressure distributions and vortex-lift characteristics of a trapezoidal wing-strake configuration / |
1 |
NAS 1.60:1291
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Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / Richmond P. Boyden, Langley Research Center. |
1 |
NAS 1.60:1292
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Laboratory and field measurements of upwelled radiance and reflectance spectra of suspended James River sediments near Hopewell, Virginia / |
1 |
NAS 1.60:1293
|
Friction and wear of metals with a single-crystal abrasive grit of silicon carbide : effect of shear strength of metal / |
1 |
NAS 1.60:1294
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Performance with and with inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region / |
1 |
NAS 1.60:1295
|
DYGABCD--a program for calculating linear A, B, C, and D matrices from a nonlinear dynamic engine simulation / |
1 |
NAS 1.60:1296
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Simulation model of a single-stage lithium bromide-water absorption cooling unit / |
1 |
NAS 1.60:1297
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Draining characteristics of hemispherically bottomed cylinders in a low-gravity environment / |
1 |
NAS 1.60:1298
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Performance of a transonic fan stage designed for a low meridional velocity ratio / |
1 |
NAS 1.60:1299
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Aerodynamic performance of a 1.35-pressure-ratio axial-flow fan stage / |
1 |
NAS 1.60:1300
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An integrated computer procedure for sizing composite airframe structures / |
1 |
NAS 1.60:1301
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A Correlation of mixing noise from coannular jets with inverted flow profiles / |
1 |