|
Y 3.N21/5:6/539
|
Aerodynamic characteristics of several airfoils of low aspect ratio / |
1 |
|
Y 3.N21/5:6/540
|
A deflection formula for single-span beams of constant section subjected to combined axial and transverse loads / |
1 |
|
Y 3.N21/5:6/541
|
The effect of the angle of afterbody keel on the water performance of a flying-boat hull model / |
1 |
|
Y 3.N21/5:6/542
|
The initial torsional stiffness of shells with interior webs / |
1 |
|
Y 3.N21/5:6/543
|
The compressibility burble / |
1 |
|
Y 3.N21/5:6/544
|
An application of the von Kármán-Millikan laminar boundary-layer theory and comparison with experiment / |
1 |
|
Y 3.N21/5:6/545
|
Tank tests of a model of a flying-boat hull having a longitudinally concave planing bottom / |
1 |
|
Y 3.N21/5:6/546
|
Comparative tests of pitot-static tubes / |
1 |
|
Y 3.N21/5:6/547
|
Development of the N.A.C.A. slot-lip aileron / |
1 |
|
Y 3.N21/5:6/548
|
Flight tests of a balanced split flap with particular reference to rapid operation / |
1 |
|
Y 3.N21/5:6/549
|
Drag of prestone and oil radiators on the YO-31A airplane / |
1 |
|
Y 3.N21/5:6/550
|
Limitations of the pilot in applying forces to airplane controls / |
1 |
|
Y 3.N21/5:6/551
|
Tank tests of three models of flying-boat hulls of the pointed-step type with different angles of dead rise - N.A.C.A. model 35 series / |
1 |
|
Y 3.N21/5:6/552
|
Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle / |
1 |
|
Y 3.N21/5:6/553
|
Notes on the technique of landing airplanes equipped with wing flaps / |
1 |
|
Y 3.N21/5:6/554
|
Circular motion of bodies of revolution / |
1 |
|
Y 3.N21/5:6/555
|
Piloting technique for recovery from spins / |
1 |
|
Y 3.N21/5:6/556
|
Further measurements of normal accelerations on racing airplanes / |
1 |
|
Y 3.N21/5:6/557
|
Considerations of the take-off problem / |
1 |
|
Y 3.N21/5:6/1266
|
Flight measurements of helicopter blade motion with a comparison between theoretical and experimental results / |
1 |
