A | B | C | D | E | F | G | H | I | J | K | L | M | N | O | P | Q | R | S | T | |
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1 | ARR # | Also released as | ||||||||||||||||||
2 | NACA-ARR-3D16 | WR-W-15 | An investigation of aircraft heaters XI : measured and predicted performance of a slotted-fin exhaust gas and air heat exchanger | |||||||||||||||||
3 | NACA-ARR-3D17 | WR-L-487 | Free-flight-tunnel investigation of the effect of the fuselage length and the aspect ratio and size of the vertical tail on lateral stability and control | |||||||||||||||||
4 | NACA-ARR-3D29 | WR-L-504 | Effect of wing leading-edge slots on the spin and recovery characteristics of airplanes | |||||||||||||||||
5 | NACA-ARR-3D30 | Landing gear design considerations | ||||||||||||||||||
6 | NACA-ARR-3E10 | WR-W-17 | An investigation of aircraft heaters XII : performance of a formed-plate crossflow exhaust gas and air heat exchanger | |||||||||||||||||
7 | NACA-ARR-3E18 | WR-W-42 | An instrument for the determination of rain densities in flight | |||||||||||||||||
8 | NACA-ARR-3E19 | WR-L-217 | Formulas for propellers in yaw and charts of the side-force derivative | |||||||||||||||||
9 | NACA-ARR-3E20 | WR-L-222 | Free-spinning-tunnel tests of a model of a canard airplane | |||||||||||||||||
10 | NACA-ARR-3E21 | WR-W-43 | Tests of exhaust propulsion nozzles | |||||||||||||||||
11 | NACA-ARR-3E22 | WR-L-458 | Jet-boundary corrections for reflection-plane models in rectangular wind tunnels | |||||||||||||||||
12 | NACA-ARR-3E24 | WR-L-330 | Method of calculating performance of dual-rotating propellers from airfoil characteristics | |||||||||||||||||
13 | NACA-ARR-3E25 | WR-L-439 | Full-scale tunnel investigation of the pressure distribution over the tail of the P-47B airplane | |||||||||||||||||
14 | NACA-ARR-3E26 | WR-E-223 | Lead susceptibility of paraffins, cycloparaffins, and olefins | |||||||||||||||||
15 | NACA-ARR-3E28 | WR-A-41 | ||||||||||||||||||
16 | NACA-ARR-3E31 | WR-L-237 | The use of a retractable planing flap instead of a fixed step on a seaplane | |||||||||||||||||
17 | NACA-ARR-3F07 | WR-L-412 | Flight tests of various tail modifications on the Brewster XSBA-1 airplane I : measurements of flying qualities with original tail surfaces | |||||||||||||||||
18 | NACA-ARR-3F12 | WR-W-67 | Some systematic model experiments on the porpoising characteristics of flying-boat hulls | |||||||||||||||||
19 | NACA-ARR-3F15 | WR-L-167 | Preliminary tank tests with planing-tail seaplane hulls | |||||||||||||||||
20 | NACA-ARR-3F16 | WR-W-64 | Fatigue characteristics of spot-welded 24S-T aluminum alloy | |||||||||||||||||
21 | NACA-ARR-3F19 | WR-W-99 | Mechanical tests of macerated phenolic molding material | |||||||||||||||||
22 | NACA-ARR-3F22 | WR-E-135 | Recommended test procedure for aircraft engine turbosupercharger power plants | |||||||||||||||||
23 | NACA-ARR-3F23 | WR-L-459 | Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V : symmetrically tapered wing with a circular fuselage having a horizontal and a vertical tail | |||||||||||||||||
24 | NACA-ARR-3F24 | WR-L-327 | Wind-tunnel vibration tests of a four-blade single rotating pusher propeller | |||||||||||||||||
25 | NACA-ARR-3F25 | WR-L-522 | Effect of wing loading and altitude on lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel | |||||||||||||||||
26 | NACA-ARR-3F28 | WR-L-387 | Experimental determination of the yawing moment due to yawing contributed by the wing, fuselage, and vertical tail of a midwing airplane model | |||||||||||||||||
27 | NACA-ARR-3F29 | WR-L-290 | Wind-tunnel investigation of control-surface characteristics XIV : NACA 0009 airfoil with a 20-percent-chord double plain flap | |||||||||||||||||
28 | NACA-ARR-3F30 | WR-L-306 | The effect of dead rise upon the high-angle porpoising characteristics of two planing surfaces in tandem | |||||||||||||||||
29 | NACA-ARR-3G06 | WR-W-66 | Some yawing tests of a 1/30-scale model of the hull of the XPB2M-1 flying boat | |||||||||||||||||
30 | NACA-ARR-3G07 | WR-W-65 | Porpoising: a comparison of theory with experiment | |||||||||||||||||
31 | NACA-ARR-3G13 | WR-L-44 | Measurements of friction coefficients in a pipe for subsonic and supersonic flow of air | |||||||||||||||||
32 | NACA-ARR-3G14 | WR-E-134 | Relation of preignition and knock to allowable engine temperatures | |||||||||||||||||
33 | NACA-ARR-3G15 | WR-L-238 | Wind-tunnel tests of four full-scale seaplane floats | |||||||||||||||||
34 | NACA-ARR-3G23 | WR-E-133 | Knocking tendency of an air-cooled aircraft-engine cylinder with one and with two spark plugs | |||||||||||||||||
35 | NACA-ARR-3G26 | WR-W-100 | Working charts for the computation of propeller thrust throughout the take-off range | |||||||||||||||||
36 | NACA-ARR-3G27 | WR-L-460 | On a function-theory method for obtaining potential-flow patterns of a compressible fluid | |||||||||||||||||
37 | NACA-ARR-3G29 | WR-L-308 | Theory of self-excited mechanical oscillations of hinged rotor blades | |||||||||||||||||
38 | NACA-ARR-3G30 | WR-L-274 | Effect of turbulence on air-flow measurements behind orifice plates | |||||||||||||||||
39 | NACA-ARR-3G31 | WR-L-341 | Design, selection, and installation of aircraft heat exchangers | |||||||||||||||||
40 | NACA-ARR-3H13 | WR-W-45 | De-icing of an aircraft-engine induction system | |||||||||||||||||
41 | NACA-ARR-3H16 | WR-L-767 | Improved baffle designs for air-cooled engine cylinders | |||||||||||||||||
42 | NACA-ARR-3H21 | WR-E-118 | A method of estimating the knock rating of hydrocarbon fuel blends | |||||||||||||||||
43 | NACA-ARR-3H23 | WR-L-506 | Wind-tunnel investigation of a full-span retractable flap in combination with full-span plain and internally balanced ailerons on a tapered wing | |||||||||||||||||
44 | NACA-ARR-3H24 | WR-A-51 | Development of thermal ice-prevention equipment for the B-17F airplane | |||||||||||||||||
45 | NACA-ARR-3H25 | WR-L-395 | Determination of the damping moment in yawing for tapered wings with partial-span flaps | |||||||||||||||||
46 | NACA-ARR-3H26 | WR-W-18 | An investigation of aircraft heaters XIII : performance of corrugated and noncorrugated fluted type exhaust gas-air heat exchangers | |||||||||||||||||
47 | NACA-ARR-3H31 | WR-L-388 | The Effect of Mass Distribution on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Free-Flight Tunnel | |||||||||||||||||
48 | NACA-ARR-3I06 | WR-W-68 | Some analyses of systematic experiments on the resistance and porpoising characteristics of flying-boat hulls | |||||||||||||||||
49 | NACA-ARR-3I10 | WR-W-59 | Protection of nonmetallic aircraft from lighting I : general analysis | |||||||||||||||||
50 | NACA-ARR-3I11 | WR-L-405 | Wind-tunnel vibration tests of dual-rotating propellers | |||||||||||||||||
51 | NACA-ARR-3I13 | WR-L-312 | Theory of mechanical oscillations of rotors with two hinged blades | |||||||||||||||||
52 | NACA-ARR-3I15 | WR-L-277 | Aerodynamic and hydrodynamic tests of a family of models of flying-boat hulls derived from a streamline body : NACA model 84 series | |||||||||||||||||
53 | NACA-ARR-3I17 | WR-W-96 | General porpoising tests on flying-boat-hull models | |||||||||||||||||
54 | NACA-ARR-3I21 | WR-L-438 | Wind tunnel investigation of rear underslung fuselage ducts | |||||||||||||||||
55 | NACA-ARR-3I25 | WR-L-286 | Representative operating charts of propellers tested in the NACA 20-foot propeller-research tunnel | |||||||||||||||||
56 | NACA-ARR-3J02 | WR-L-368 | Stresses around rectangular cut-outs in skin-stringer panels under axial loads II | |||||||||||||||||
57 | NACA-ARR-3J04 | WR-L-557 | Data on buckling strength of curved sheet in compression | |||||||||||||||||
58 | NACA-ARR-3J07 | WR-E-128 | The Measurement of Fuel-Air Ratio by Analysis of the Oxidized Exhaust Gas | |||||||||||||||||
59 | NACA-ARR-3J11 | WR-W-46 | Effect of pH on strength of resin bonds | |||||||||||||||||
60 | NACA-ARR-3J12 | WR-W-60 | Protection of nonmetallic aircraft from lightning II : lightning conductor materials | |||||||||||||||||
61 | NACA-ARR-3J13 | WR-L-407 | Wind-tunnel investigation of wing ducts on a single engine pursuit airplane | |||||||||||||||||
62 | NACA-ARR-3J18 | WR-L-354 | Free-flight-tunnel investigation of the effect of mode of propeller rotation upon the lateral-stability characteristics of a twin-engine airplane model with single vertical tails of different size | |||||||||||||||||
63 | NACA-ARR-3J22 | WR-L-322 | The design of cooling ducts with special reference to the boundary layer at the inlet | |||||||||||||||||
64 | NACA-ARR-3J23 | WR-L-358 | Effect of length-beam ration on resistance and spray of three models of flying-boat hulls | |||||||||||||||||
65 | NACA-ARR-3J27 | WR-L-466 | Critical stresses for plates | |||||||||||||||||
66 | NACA-ARR-3J28 | WR-L-311 | Wind-tunnel tests of two tapered wings with straight leading edges and with constant-chord center sections of different spans | |||||||||||||||||
67 | NACA-ARR-3J29 | Estimation of stick forces from wind-tunnel aileron data | ||||||||||||||||||
68 | NACA-ARR-3K01 | WR-L-209 | Experimental Investigation of Entrance-Region Heat-Transfer Coefficients | |||||||||||||||||
69 | NACA-ARR-3K02 | WR-L-320 | Kaplan | |||||||||||||||||
70 | NACA-ARR-3K04 | WR-L-429 | Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel and rectangular-tube section | |||||||||||||||||
71 | NACA-ARR-3K06 | WR-L-326 | Principles of moment distribution applied to stability of structures composed of bars or plates | |||||||||||||||||
72 | NACA-ARR-3K08 | WR-L-410 | Design criterions for the dimensions of the forebody of a long-range flying boat | |||||||||||||||||
73 | NACA-ARR-3K10 | WR-A-49 | Flight tests of thermal ice-prevention equipment on a Lockheed 12A airplane | |||||||||||||||||
74 | NACA-ARR-3K11 | WR-W-69 | A method for making quantitative studies of the main spray characteristics of flying-boat hull models | |||||||||||||||||
75 | NACA-ARR-3K12 | WR-L-476 | Critical shear stress of an infinitely long flat plate with equal elastic restraints against rotation along the parallel edges | |||||||||||||||||
76 | NACA-ARR-3K13 | WR-L-340 | Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress | |||||||||||||||||
77 | NACA-ARR-3K15 | WR-L-413 | A comparative study of the effect of wing flutter shape on the critical flutter speed | |||||||||||||||||
78 | NACA-ARR-3K16 | WR-A-64 | A flight investigation of fuselage static-pressure-vent airspeed installations | |||||||||||||||||
79 | NACA-ARR-3K17 | WR-L-372 | Theoretical analysis of the lateral stability of a glider towed by twin parallel towlines | |||||||||||||||||
80 | NACA-ARR-3K27 | WR-L-398 | Tables of stiffness and carry-over factor for flat rectangular plates under compression | |||||||||||||||||
81 | NACA-ARR-3L01 | WR-W-61 | Fatigue strength and related characteristics of spot-welded joints in 24S-T alclad sheet | |||||||||||||||||
82 | NACA-ARR-3L02 | WR-L-370 | Tests of inverted spins in the NACA free-spinning tunnels | |||||||||||||||||
83 | NACA-ARR-3L03 | WR-E-122 | Construction of wire strain gages for engine application | |||||||||||||||||
84 | NACA-ARR-3L04 | WR-W-71 | Some systematic model experiments of the bow-spray characteristics of flying-boat hulls operating at low speeds in waves | |||||||||||||||||
85 | NACA-ARR-3L06 | WR-E-140 | Operating Temperatures of a Sodium-Cooled Exhaust Valve as Measured by a Thermocouple | |||||||||||||||||
86 | NACA-ARR-3L07 | WR-L-272 | Flight tests of F2A-2 airplane with full-span slotted flaps and trailing-edge and slot-lip ailerons | |||||||||||||||||
87 | NACA-ARR-3L08 | WR-L-349 | Methods and charts for computing stability derivatives of a v-bottom planing surface | |||||||||||||||||
88 | NACA-ARR-3L09 | WR-L-219 | Propellers in yaw | |||||||||||||||||
89 | NACA-ARR-3L10 | WR-L-469 | Wind-tunnel investigation of an NACA 23012 airfoil with a 0.30-airfoil-chord double slotted flap | |||||||||||||||||
90 | NACA-ARR-3L14 | WR-E-127 | Correlation of single-cylinder cooling tests of a Pratt and Whitney R-2800-21 engine cylinder with wind-tunnel tests of a Pratt and Whitney R-2800-27 engine | |||||||||||||||||
91 | NACA-ARR-4A01 | WR-W-102 | A method for welding sheet aluminum to SAE 4140 steel | |||||||||||||||||
92 | NACA-ARR-4A05 | WR-L-482 | Shear-lag tests of two box beams with corrugated covers loaded to failure | |||||||||||||||||
93 | NACA-ARR-4A06 | WR-L-361 | A theoretical investigation of the rolling oscillations of an airplane with ailerons free | |||||||||||||||||
94 | NACA-ARR-4A07 | WR-L-313 | Garrick | |||||||||||||||||
95 | NACA-ARR-4A08 | WR-A-42 | Heaslet | |||||||||||||||||
96 | NACA-ARR-4A11 | WR-A-10 | Analysis of a thermal ice-prevention system for wing leading-edge landing-light installations | |||||||||||||||||
97 | NACA-ARR-4A18 | WR-L-310 | Comparison of an approximate and an exact method of shear-lag analysis | |||||||||||||||||
98 | NACA-ARR-4A20 | WR-A-47 | Tests of Thermal-Electric De-Icing Equipment for Propellers | |||||||||||||||||
99 | NACA-ARR-4A21 | WR-W-19 | An investigation of aircraft heaters XV : the emissivity of several materials | |||||||||||||||||
100 | NACA-ARR-4A22 | WR-L-457 | Effects of heat-capacity lag in gas dynamics |