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Y 3.N 21/5:6/3469
|
Summary of results obtained by transonic-bump method on effects of plan form and thickness on lift and drag characteristics of wings at transonic speeds / |
1 |
|
Y 3.N 21/5:6/3470
|
Gust-tunnel investigation of the effect of a sharp-edge gust on the flapwise blade bending moments of a model helicopter rotor / |
1 |
|
Y 3.N 21/5:6/3471
|
Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds / |
1 |
|
Y 3.N 21/5:6/3472
|
Flow studies on flat-plate delta wings at supersonic speed / |
1 |
|
Y 3.N 21/5:6/3473
|
Effects of sweep and angle of attack on boundary-layer transition on wings at Mach number 4.04 / |
1 |
|
Y 3.N 21/5:6/3474
|
Rapid radiant-heating tests of multiweb beams / |
1 |
|
Y 3.N 21/5:6/3475
|
An analysis of acceleration, airspeed, and gust-velocity data from one type of four-engine transport airplane operated over two domestic routes / |
2 |
|
Y 3.N 21/5:6/3476
|
Calculated spanwise lift distributions and aerodynamic influence coefficients for swept wings in subsonic flow / |
1 |
|
Y 3.N 21/5:6/3477
|
Hydrodynamic pressure distributions obtained during a planing investigation of five related prismatic surfaces / |
1 |
|
Y 3.N 21/5:6/3478
|
On boattail bodies of revolution having minimum wave drag / |
1 |
|
Y 3.N 21/5:6/3479
|
Analysis of the horizontal-tail loads measured in flight on a multiengine jet bomber / |
1 |
|
Y 3.N 21/5:6/3480
|
Free-spinning-tunnel investigation of gyroscopic effects of jet-engine rotating parts (or of rotating propellers) on spin and spin recovery / |
1 |
|
Y 3.N 21/5:6/3481
|
Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6 / |
1 |
|
Y 3.N 21/5:6/3482
|
Supplementary charts for estimating performance of high-performance helicopters / |
1 |
|
Y 3.N 21/5:6/3483
|
An analysis of acceleration, airspeed, and gust-velocity data from a four-engine transport airplane in operations on an eastern United States route / |
2 |
|
Y 3.N 21/5:6/3484
|
On spectral analysis of runway roughness and loads developed during taxiing / |
1 |
|
Y 3.N 21/5:6/3485
|
An approximate solution for axially symmetric flow over a cone with an attached shock wave / |
1 |
|
Y 3.N 21/5:6/3486
|
Measurements of turbulent skin friction on a flat plate at transonic speeds / |
1 |
|
Y 3.N 21/5:6/3487
|
Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces / |
2 |
|
Y 3.N 21/5:6/3488
|
Some measurements of flow in a rectangular cutout / |
1 |
