| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:6/712 |
A preliminary study of the prevention of ice on aircraft by the use of engine-exhaust heat / A preliminary study of the prevention of ice on aircraft by the use of engine℗--exhaust heat. A Preliminary study of the prevention of ice on aircraft by the use of engine-exhaust heat / |
3 |
| Y 3.N 21/5:6/713 |
A comparison of several tapered wings designed to avoid tip stalling / A comparison of several tapered wings designed to avoid tip stalling. A Comparison of several tapered wings designed to avoid tip stalling / |
3 |
| Y 3.N 21/5:6/714 |
Flight tests of retractable ailerons on a highly tapered wing / Flight tests of retractable ailerons on a highly tapered wing. |
3 |
| Y 3.N 21/5:6/715 |
Wind-tunnel investigation of an N.A.C.A. 23012 airfoil with two arrangements of a wide-chord slotted flap / Wind-tunnel investigation of N. A. C. A. 23012 airfoil with two arrangements of a wide-chord slotted flap. |
3 |
| Y 3.N 21/5:6/716 |
Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise : N.A.C.A. models 57-A, 57-B, and 57-C / Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise, N. A. C. A. models 57-A, 57-B, and 57-C. Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise. : N.A.C.A. models 57-A, 57-B, and 57-C / |
3 |
| Y 3.N 21/5:6/717 |
A method of estimating the critical buckling load for structural members / A method of estimating the critical buckling load for structural members. A Method of estimating the critical buckling load for structural members / |
3 |
| Y 3.N 21/5:6/718 |
Resistance of transparent plastics to impact / Resistance of transparent plastics to impact. |
3 |
| Y 3.N 21/5:6/719 |
The effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N.A.C.A. 23012 wing / The effects of partial℗--span slotted flaps on aerodynamic characteristics of a rectangular and a tapered N. A. C. A. 23012 wing. The Effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and tapered N.A.C.A. 23012 wing / |
3 |
| Y 3.N 21/5:6/720 |
Flight tests of N.A.C.A. nose-slot cowlings on the BFC-1 airplane / Flight tests of N. A. C. A. nose℗--slot cowlings on the BFC-1 airplane. |
3 |
| Y 3.N 21/5:6/721 |
Compressive tests of a monocoque box / Compressive tests of a monocoque box. |
3 |
| Y 3.N 21/5:6/722 |
Local instability of centrally loaded columns of channel section and Z-section / Local instability of centrally loaded columns of channel section and Z℗--section. |
3 |
| Y 3.N 21/5:6/723 |
Adhesion of ice in its relation to the de-icing of airplanes / Adhesion of ice in its relation to de℗--icing of airplanes. |
3 |
| Y 3.N 21/5:6/724 |
The effects of surface waviness and of rib stitching on wing drag / The effects of surface waviness and of rib stitching on wing drag. The Effects of surface waviness and of rib stitching on wing drag / |
3 |
| Y 3.N 21/5:6/725 |
Tank tests to determine the effects of the chine flare of a flying-boat hull : N.A.C.A. model series 62 and 69 / Tank tests to determine the effects of the chine flare of a flying-boat hull. : N.A.C.A. model series 62 and 69 / Tank tests to determine the effects of the chine flare of a flying-boat hull, N. A. C. A. model series 62 and 69. |
3 |
| Y 3.N 21/5:6/726 |
Combined beam-column stresses of aluminum-alloy channel sections / Combined beam℗--column stresses of aluminum-alloy channel sections. |
3 |
| Y 3.N 21/5:6/727 |
A flight investigation of the distribution of ice-inhibiting fluids on a propeller blade / A Flight investigation of the distribution of ice-inhibiting fluids on a propeller blade / A flight investigation of the distribution of ice℗--inhibiting fluids on a propeller blade. |
3 |
| Y 3.N 21/5:6/728 |
Wind-tunnel investigation of an N.A.C.A. 23021 airfoil with two arrangements of a 40-percent-chord slotted flap / Wind-tunnel investigation of N. A. C. A. 23021 airfoil with two arrangements of 40-percent-chord slotted flap. |
3 |
| Y 3.N 21/5:6/729 |
An instrument for estimating tautness of doped fabrics on aircraft / An instrument for estimating tautness of doped fabrics on aircraft. An Instrument for estimating tautness of doped fabrics on aircraft / |
3 |
| Y 3.N 21/5:6/730 |
Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. Wind℗--tunnel investigation of effect of yaw on lateral℗--stability characteristics, II--Rectangular N. A. C. A. 23012 wing with a circular fuselage and fin. Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. : 2 - Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin / |
3 |
| Y 3.N 21/5:6/731 |
Tests in the gust tunnel of a model of the XBM-1 airplane / Tests in the gust tunnel of a model of the XBM-1 airplane. |
3 |
