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Y 3.N 21/5:6/1620
|
The Calculation of downwash behind supersonic wings with an application to triangular plan forms / |
1 |
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Y 3.N 21/5:6/1621
|
Two-dimensional unstead lift problems in supersonic flight / |
1 |
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Y 3.N 21/5:6/1622
|
Analysis and preliminary design of an optical instrument for the measurement of drop size and free-water content of clouds / |
2 |
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Y 3.N 21/5:6/1623
|
Some fundamental similarities between boundary-layer flow at transonic and low speeds / |
1 |
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Y 3.N 21/5:6/1624
|
Two-dimensional wind-tunnel investigation of an NACA 64-009 airfoil with two types of leading-edge flap / |
1 |
|
Y 3.N 21/5:6/1625
|
Observations on the maximum average stress of flat plates buckled in edge compression / |
1 |
|
Y 3.N 21/5:6/1626
|
A Study of ceramic coatings for high-temperature protection of molybdenum / |
1 |
|
Y 3.N 21/5:6/1627
|
Effect of steady rolling on longitudinal and directional stability / |
1 |
|
Y 3.N 21/5:6/1628
|
An Analysis of the variation with altitude of effective gust velocity in convective-type clouds / |
1 |
|
Y 3.N 21/5:6/1629
|
The Experimental determination of the moments of inertia of airplanes by a simplified compound-pendulum method / |
1 |
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Y 3.N 21/5:6/1630
|
A Generalized theoretical investigation of the hydrodynamic pitching moments experienced by V-bottom seaplanes during step-landing impacts and comparisons with experiment / |
1 |
|
Y 3.N 21/5:6/1631
|
Wind-tunnel investigation of boundary-layer control by suction on NACA 65₅-424 airfoil with double slotted flap / |
1 |
|
Y 3.N 21/5:6/1632
|
Gust-tunnel testing to determine influence of airfoil section characteristics on gust-load factors / |
1 |
|
Y 3.N 21/5:6/1633
|
An Evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil section wit a special mean-camber line designed to produce a high critical Mach number / |
1 |
|
Y 3.N 21/5:6/1634
|
Wind-tunnel tests and analysis of two 10-foot-diameter six-blade dual-rotating tractor propellers differing in pitch distribution / |
1 |
|
Y 3.N 21/5:6/1635
|
Strength tests of shear webs with uprights not connected to the flanges / |
1 |
|
Y 3.N 21/5:6/1636
|
Determination of stresses in gas-turbine disks subjected to plastic flow and creep / |
1 |
|
Y 3.N 21/5:6/1637
|
Effect of preignition on cylinder temperatures, pressures, power output, and piston failures / |
1 |
|
Y 3.N 21/5:6/1638
|
Experimental investigation of the jet-boundary constriction correction for a model spanning a closed circular tunnel / |
1 |
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Y 3.N 21/5:6/1639
|
Investigation of some factors affecting comparisons of wind-tunnel and flight measurements of maximum lift coefficients for a fighter-type airplane / |
1 |
