Y 3.N 21/5:6/4182
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Physical characteristics and test conditions of an ethylene-heated high-temperature jet / |
1 |
Y 3.N 21/5:6/4183
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Investigation of effects of distributed surface roughness on a turbulent boundary layer over a body of revolution at a Mach number of 2.01 / |
1 |
Y 3.N 21/5:6/4184
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Measurement of static pressure on aircraft / |
1 |
Y 3.N 21/5:6/4185
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Wind-tunnel investigation of effect of sweep on rolling derivatives at angles of attack up to 13 degrees and at high subsonic Mach numbers, including a semiempirical method of estimating the rolling derivatives / |
1 |
Y 3.N 21/5:6/4186
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Heat transfer in isotropic turbulence during the final period of decay / |
1 |
Y 3.N 21/5:6/4187
|
High-speed hydrodynamic characteristics of a flat plate and 20 degree dead-rise surface in unsymmetrical planing conditions / |
1 |
Y 3.N 21/5:6/4188
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Charts relating the compressive and shear buckling stresses of longitudinally supported plates to the effective deflectional stiffness of the supports / |
1 |
Y 3.N 21/5:6/4189
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Lift and moment on thin arrowhead wings with supersonic edges oscillating in symmetric flapping and roll and application to the flutter of an all-movable control surface / |
1 |
Y 3.N 21/5:6/4190
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Experimental investigation of the lateral trim of a wing-propeller combination at angles of attack up to 90 degrees with all propellers turning in the same direction / |
1 |
Y 3.N 21/5:6/4191
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Analysis of horizontal-tail loads in pitching maneuvers on a flexible swept-wing jet bomber / |
1 |
Y 3.N 21/5:6/4192
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Three-degree-of-freedom evaluation of the longitudinal transfer functions of a supersonic canard missile configuration including changes in forward speed / |
1 |
Y 3.N 21/5:6/4193
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Subsonic flight investigation of methods to improve the damping of lateral oscillations by means of a viscous damper in the rudder system in conjuction with adjusted hinge-moment parameters / |
1 |
Y 3.N 21/5:6/4194
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Comparison of hydrodynamic-impact acceleration and response for systems with single and with multiple elastic modes / |
1 |
Y 3.N 21/5:6/4195
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Shape of initial portion of boundary of supersonic axisymmetric free jets at large jet pressure ratios / |
1 |
Y 3.N 21/5:6/4196
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A method for the calculation of the lateral response of airplanes to random turbulence / |
1 |
Y 3.N 21/5:6/4197
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Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles / |
1 |
Y 3.N 21/5:6/4198
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Effects of airplane flexibility on wing strains in rough air at 35,000 feet as determined by a flight investigation of a large swept-wing airplane / |
1 |
Y 3.N 21/5:6/4199
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A flight investigation of the effects of varied lateral damping on the effectiveness of a fighter airplane as a gun platform / |
1 |
Y 3.N 21/5:6/4200
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Effectiveness of boundary-layer control, obtained by blowing over a plain rear flap in combination with a forward slotted flap, in deflecting a slipstream downward for vertical take-off / |
1 |
Y 3.N 21/5:6/4201
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Collection of zero-lift drag data on bodies of revolution from free-flight investigations / |
1 |