A | B | C | D | E | F | |
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1 | NACA-TN-1 | Notes on longitudinal stability and balance | Image harvested from NTRS | |||
2 | NACA-TN-2 | Airplane performance as influenced by the use of a supercharged engine | Image harvested from NTRS | |||
3 | NACA-TN-3 | Notes on the theory of the accelerometer | Image harvested from NTRS | |||
4 | NACA-TN-4 | The problem of the helicopter | Image harvested from NTRS | |||
5 | NACA-TN-5 | Relation of rib spacing to stress in wing planes | Image harvested from NTRS | |||
6 | NACA-TN-6 | Static testing and proposed standard specifications | Image harvested from NTRS | |||
7 | NACA-TN-7 | Notes on the design of supercharged and overdimensioned aircraft engines | Image harvested from NTRS | |||
8 | NACA-TN-8 | Duralumin | Image harvested from NTRS | |||
9 | NACA-TN-9 | Theory of lifting surfaces | Image harvested from NTRS | |||
10 | NACA-TN-10 | The law relating to air currents | Image harvested from NTRS | |||
11 | NACA-TN-10-Pt-2 | Theory of Lifting Surfaces, Part 2 | Image harvested from NTRS | |||
12 | NACA-TN-11 | The problem of the turbo-compressor | Image harvested from NTRS | |||
13 | NACA-TN-12 | Recent efforts and experiments in the construction of aviation engines | Image harvested from NTRS | |||
14 | NACA-TN-13 | Soaring flight in Guinea | Image harvested from NTRS | |||
15 | NACA-TN-14 | Increase in maximum pressures produced by preignition in internal combustion engines | Image harvested from NTRS | |||
16 | NACA-TN-15 | Tests of the Daimler D-IVa engine at a high altitude test bench | Image harvested from NTRS | |||
17 | NACA-TN-16 | Experience with geared propeller drives for aviation engines | Image harvested from NTRS | |||
18 | NACA-TN-17 | Italian and French experiments on wind tunnels | Image harvested from NTRS | |||
19 | NACA-TN-18 | The dynamometer hub | Image harvested from NTRS | |||
20 | NACA-TN-19 | The steadiness factor in engine sets | Image harvested from NTRS | |||
21 | NACA-TN-20 | Notes on specifications for French airplane competitions | Image harvested from NTRS | |||
22 | NACA-TN-21 | Drag or negative traction of geared-down supporting propellers in the downward vertical glide of a helicopter | Image harvested from NTRS | |||
23 | NACA-TN-22 | The photographic recording of small motions | Image harvested from NTRS | |||
24 | NACA-TN-23 | Horizontal buoyancy in wind tunnels | Image harvested from NTRS | |||
25 | NACA-TN-24 | Development of the inflow theory of the propeller | Image harvested from NTRS | |||
26 | NACA-TN-25 | Center of pressure coefficients for airfoils at high speeds | Image harvested from NTRS | |||
27 | NACA-TN-26 | A variable speed fan dynamometer | Image harvested from NTRS | |||
28 | NACA-TN-27 | Instrument for measuring engine clearance volumes | Image harvested from NTRS | |||
29 | NACA-TN-28 | Loads and calculations of army airplanes | Image harvested from NTRS | |||
30 | NACA-TN-29 | Progress made in the construction of giant airplanes in Germany during the war | Image harvested from NTRS | |||
31 | NACA-TN-30 | Design of recording wind tunnel balances | Image harvested from NTRS | |||
32 | NACA-TN-31 | Crippling strength of axially loaded rods | Image harvested from NTRS | |||
33 | NACA-TN-32 | Causes of cracking of ignition cable | Image harvested from NTRS | |||
34 | NACA-TN-33 | The effect of the nature of surfaces on resistance as tested on struts | Image harvested from NTRS | |||
35 | NACA-TN-34 | The 300 H.P. Benz aircraft engine | Image harvested from NTRS | |||
36 | NACA-TN-35 | The optical wing aligning device of the Langley Field tunnel | Image harvested from NTRS | |||
37 | NACA-TN-36 | N.A.C.A. Langley field wind tunnel apparatusthe tilting manometer | Image harvested from NTRS | |||
38 | NACA-TN-37. | The determination of the effective resistance of a spindle supporting a model airfoil | Image harvested from NTRS | |||
39 | NACA-TN-38 | Measurements of rudder moments on an airplane during flight | Image harvested from NTRS | |||
40 | NACA-TN-39 | High thermal efficiency in airplane service | Image harvested from NTRS | |||
41 | NACA-TN-40 | Effect of the reversal of air flow upon the discharge coefficient of Durley Orifices | Image harvested from NTRS | |||
42 | NACA-TN-41 | Influence of span and load per square meter on the air forces of the supporting surface | Image harvested from NTRS | |||
43 | NACA-TN-42 | The determination of downwash | Image harvested from NTRS | |||
44 | NACA-TN-43 | Note on the resistance of polished cylinders (and cylindrical wires) with generatrices perpendicular to the airstream | Image harvested from NTRS | |||
45 | NACA-TN-44 | On the Resistance of spheres and ellipsoids in wind tunnels | Image harvested from NTRS | |||
46 | NACA-TN-45 | Extract from a report on the resistance of spheres of small diameter in an airstream of high velocity | Image harvested from NTRS | |||
47 | NACA-TN-46 | Theory of the ideal windmill | Image harvested from NTRS | |||
48 | NACA-TN-47 | Recent European developments in helicopters | Image harvested from NTRS | |||
49 | NACA-TN-48 | Airplane superchargers | Image harvested from NTRS | |||
50 | NACA-TN-49 | On the resistance of the air at high speeds and on the automatic rotation of projectiles | Image harvested from NTRS | |||
51 | NACA-TN-50 | Gordon Bennett Airplane Cup | Image harvested from NTRS | |||
52 | NACA-TN-51 | Airplane balance | Image harvested from NTRS | |||
53 | NACA-TN-52 | A new method of testing in wind tunnels | Image harvested from NTRS | |||
54 | NACA-TN-53 | Similitude tests on wind sections | Image harvested from NTRS | |||
55 | NACA-TN-54 | The factors that determine the minimum speed of an airplane | Image harvested from NTRS | |||
56 | NACA-TN-55 | Airplane crashes: engine troubles : a possible explanation | Image harvested from NTRS | |||
57 | NACA-TN-56 | The development of German Army airplanes during the war | Image harvested from NTRS | |||
58 | NACA-TN-57 | The Caproni Seaplane | Image harvested from NTRS | |||
59 | NACA-TN-58 | Absolute coefficients and the graphical representation of airfoil characteristics | Image harvested from NTRS | |||
60 | NACA-TN-59 | The dynamometer hub for the testing propellers and engines during flight | Image harvested from NTRS | |||
61 | NACA-TN-60 | On a new type of wind tunnel | Image harvested from NTRS | |||
62 | NACA-TN-61 | Performance of a vane driven-gear pump | Image harvested from NTRS | |||
63 | NACA-TN-62 | The problem of fuel for aviation engines | Image harvested from NTRS | |||
64 | NACA-TN-63 | The employment of airships for the transport of passengers | Image harvested from NTRS | |||
65 | NACA-TN-64 | N.A.C.A. recording air speed meter | Image harvested from NTRS | |||
66 | NACA-TN-65 | Langley Field wind tunnel apparatus | Image harvested from NTRS | |||
67 | NACA-TN-66 | Gottingen Wind Tunnel for testing aircraft models | Image harvested from NTRS | |||
68 | NACA-TN-67 | Ground influence on airfoils | Image harvested from NTRS | |||
69 | NACA-TN-68 | Vortices and the related principles of hydrodynamics | Image harvested from NTRS | |||
70 | NACA-TN-69 | An investigation on the effect of raked wing tips | Image harvested from NTRS | |||
71 | NACA-TN-70 | The effect of staggering a biplane | Image harvested from NTRS | |||
72 | NACA-TN-71 | Experiments wit slotted wings | Image harvested from NTRS | |||
73 | NACA-TN-72 | Aneroid investigations in Germany | Image harvested from NTRS | |||
74 | NACA-TN-73 | The choice of wing sections for airplanes | Image harvested from NTRS | |||
75 | NACA-TN-74 | Mutual influence of wings and propeller | Image harvested from NTRS | |||
76 | NACA-TN-75 | Effects of varying the relative vertical position of wing and fuselage | Image harvested from NTRS | |||
77 | NACA-TN-76 | A mechanical device for illustrating airplane stability | Image harvested from NTRS | |||
78 | NACA-TN-77 | A preliminary investigation of a new method for testing aerofoils in free flight | Image harvested from NTRS | |||
79 | NACA-TN-78 | Impact tests for woods | Image harvested from NTRS | |||
80 | NACA-TN-79 | Effect of aerofoil aspect ratio on the slope of the lift curve | Image harvested from NTRS | |||
81 | NACA-TN-80 | The dead weight of the airship and the number of passengers that can be carried | Image harvested from NTRS | |||
82 | NACA-TN-81 | Langley Field wind tunnel apparatus | Image harvested from NTRS | |||
83 | NACA-TN-82 | Notes on the construction and testing of model airplanes | Image harvested from NTRS | |||
84 | NACA-TN-83 | The theory of the screw propeller | Image harvested from NTRS | |||
85 | NACA-TN-84 | New data on the laws of fluid resistance | Image harvested from NTRS | |||
86 | NACA-TN-85 | Air force and three moments for F-5-L Seaplane | Image harvested from NTRS | |||
87 | NACA-TN-86 | Surface area coefficients for airship envelopes | Image harvested from NTRS | |||
88 | NACA-TN-87 | Hydrostatic tests of an airship model | Image harvested from NTRS | |||
89 | NACA-TN-88 | Tests of oil scraper piston ring and piston fitted with oil drain holes | Image harvested from NTRS | |||
90 | NACA-TN-89 | The choice of the speed of an airship | Image harvested from NTRS | |||
91 | NACA-TN-90 | Syphon diaphragms : a method for predicting their performance for purposes of instrument design | Image harvested from NTRS | |||
92 | NACA-TN-91 | Notes on propeller design I : the energy losses of the propeller | Image harvested from NTRS | |||
93 | NACA-TN-92 | Full scale determination of the lift and drag of a seaplane | Image harvested from NTRS | |||
94 | NACA-TN-93 | The background of detonation | Image harvested from NTRS | |||
95 | NACA-TN-94 | Notes on propeller design | Image harvested from NTRS | |||
96 | NACA-TN-95 | Notes on propeller design III | Image harvested from NTRS | |||
97 | NACA-TN-96 | Notes on propeller design IV : general proceeding in design | Image harvested from NTRS | |||
98 | NACA-TN-97 | N.A.C.A. control position recorder | Image harvested from NTRS | |||
99 | NACA-TN-98 | Notes on the design of latticed columns subject to lateral loads | Image harvested from NTRS | |||
100 | NACA-TN-99 | Notes on the standard atmosphere | Image harvested from NTRS |