Y 3.N 21/5:6/3730
|
The interference effects of a body on the spanwise load distributions of two 45 degree sweptback wings of aspect ratio 8.02 from low-speed tests / |
1 |
Y 3.N 21/5:6/3731
|
Tensile properties of Inconel and RS-120 titanium-alloy sheet under rapid-heating and constant-temperature conditions / |
1 |
Y 3.N 21/5:6/3732
|
An investigation of vertical-wind-shear intensities from balloon soundings for application to airplane- and missile-response problems / |
1 |
Y 3.N 21/5:6/3733
|
Probability and frequency characteristics of some flight buffet loads / |
1 |
Y 3.N 21/5:6/3734
|
Turbulent-heat-transfer measurements at a Mach number of 3.90 / |
1 |
Y 3.N 21/5:6/3735
|
Bending tests of ring-stiffened circular cylinders / |
1 |
Y 3.N 21/5:6/3736
|
Poisson's ratios and volume changes for plastically orthotropic material / |
1 |
Y 3.N 21/5:6/3737
|
The motions of rolling symmetrical missiles referred to a body-axis system / |
1 |
Y 3.N 21/5:6/3738
|
Theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tails of vortex-induced velocities / |
1 |
Y 3.N 21/5:6/3739
|
Flight investigation of the performance of a two-stage solid-propellant Nike-Deacon (DAN) meteorological sounding rocket / |
1 |
Y 3.N 21/5:6/3740
|
Preliminary wind-tunnel tests of triangular and rectangular wings in steady roll at Mach numbers of 1.62 and 1.92 / |
1 |
Y 3.N 21/5:6/3741
|
An investigation of the loads on the vertical tail of a jet-bomber airplane resulting from flight through rough air / |
1 |
Y 3.N 21/5:6/3742
|
Tensile properties of HK31XA-H24 magnesium-alloy sheet under rapid-heating conditions and constant elevated temperatures / |
1 |
Y 3.N 21/5:6/3743
|
An optimum switching criterion for a third-order contactor acceleration control system / |
1 |
Y 3.N 21/5:6/3744
|
Supersonic flow past nonlifting bumped and indented bodies of revolution / |
1 |
Y 3.N 21/5:6/3745
|
Transition-flight tests of a model of a low-wing transport vertical-take-off airplane with tilting wing and propellers / |
1 |
Y 3.N 21/5:6/3746
|
Initial results of a flight investigation of the wing and tail loads on an airplane equipped with a vane-controlled gust-alleviation system / |
1 |
Y 3.N 21/5:6/3747
|
Equations and procedures for numerically calculating the aerodynamic characteristics of lifting rotors / |
1 |
Y 3.N 21/5:6/3748
|
Calculation and compilation of the unsteady-lift functions for a rigid wing subjected to sinusoidal gusts and to sinusoidal sinking oscillations / |
1 |
Y 3.N 21/5:6/3749
|
Torsional stiffness of thin-walled shells having reinforcing cores and rectangular, triangular or diamond cross section / |
1 |