| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:6/652 |
Tables of stiffness and carry-over factor for structural members under axial load / Tables of stiffness and carry-over factor for structural members under axial load. |
3 |
| Y 3.N 21/5:6/653 |
A flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design / Flight investigation of reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design. |
3 |
| Y 3.N 21/5:6/654 |
Fuel consumption of a carburetor engine at various speeds and torques / Fuel consumption of carburetor engine at various speeds and torques. |
3 |
| Y 3.N 21/5:6/655 |
Principles involved in the cooling of a finned and baffled cylinder / Principles involved in cooling of finned and baffled cylinder. |
3 |
| Y 3.N 21/5:6/656 |
Hydrodynamic and aerodynamic tests of models of floats for single-float seaplanes, N.A.C.A. models 41-D, 41-E, 61-A, 73, and 73-A / Hydrodynamic and aerodynamic tests of models of floats for single℗--float seaplanes. N. A. C. A. models 41-D. 41-E. 61-A. 73 and 73-A. Hydrodynamic and aerodynamic tests of models of floats for single-float seaplanes. : N.A.C.A. models 41-D, 41-E, 61-A, 73, and 73-A / |
3 |
| Y 3.N 21/5:6/657 |
Tank tests to show the effect of rivet heads on the water performance of a seaplane float / Tank tests to show effect of rivet heads on water performance of seaplane float. |
3 |
| Y 3.N 21/5:6/658 |
Generalized analysis of experimental observations in problems of elastic stability / Generalized analysis of experimental observations in problems of elastic stability. |
3 |
| Y 3.N 21/5:6/659 |
Wind-tunnel tests of three lateral-control devices in combination with a full-span slotted flap on an N.A.C.A. 23012 airfoil / Wind℗--tunnel tests of 3 lateral-control devices in combination with full℗--span slotted flap on N. A. C. A. 23012 airfoil. |
3 |
| Y 3.N 21/5:6/660 |
Fatigue testing of wing beams by the resonance method / Fatigue testing of wing beams by resonance method. |
3 |
| Y 3.N 21/5:6/661 |
Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plain ailerons and full-span split flaps / Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plaine ailerons and full-span split flaps / |
2 |
| Y 3.N 21/5:6/662 |
Gyroscopic instruments for instrument flying / Gyroscopic instruments for instrument flying. |
3 |
| Y 3.N 21/5:6/663 |
The effects of partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y-wing / The Effects of partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y wing / |
2 |
| Y 3.N 21/5:6/664 |
Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. : III. Mass distributed along the wings / Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails, III. Mass distributed along the wings. |
3 |
| Y 3.N 21/5:6/665 |
Tests of N-85, N-86, and N-87 airfoil sections in the 11-inch high-speed wind tunnel / Tests of N-85, N-86, and N-87 airfoil sections in 11-inch high-speed wind tunnel. |
3 |
| Y 3.N 21/5:6/666 | Longitudinal stability in relation to the use of an automatic pilot / | 2 |
| Y 3.N 21/5:6/667 |
Operational treatment of the nonuniform-lift theory in airplane dynamics / Operational treatment of nonuniform-lift theory in airplane dynamics. |
3 |
| Y 3.N 21/5:6/668 |
Hydrodynamic and aerodynamic tests of models of flying-boat hulls designed for low aerodynamic drag, N.A.C.A. Models 74, 74-A, and 75 / Longitudinal stability in relation to use of automatic pilot. Hydrodynamic and aerodynamic tests of models of flyingboat hulls designed for low aerodynamic drag. Hydrodynamic and aerodynamic tests of models of flying-boat hulls designed for low aerodynamic drag. : N.A.C.A. Models 74, 74-A, and 75 / |
4 |
| Y 3.N 21/5:6/669 |
The drag of inflatable rubber de-icers / The drag of inflatable rubber de-icers. The Drag of inflatable rubber de-icers / |
3 |
| Y 3.N 21/5:6/670 |
N.A.C.A. stall-warning indicator / N.A.C.A. Stall-warning indicator. |
3 |
| Y 3.N 21/5:6/671 |
A method of rapidly estimating the position of the laminar separation point / Method of rapidly estimating position of laminar separation point. A Method of rapidly estimating the position of the laminar separation point / |
3 |
