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1 | NACA-RM-50J19 | Effects of molding conditions on some physical properties of glass-fabric unsaturated-polyester laminates | Image harvested from NTRS | |||
2 | NACA-RM-51A04 | Cooperative investigation of relationship between static and fatigue properties of heat-resistant alloys at elevated temperatures | Image harvested from NTRS | |||
3 | NACA-RM-51B05 | Properties of low-carbon N-155 alloy bar stock from 1200 to 1800 F | Image harvested from NTRS | |||
4 | NACA-RM-51B23 | The properties of three cast polyester resins of Sierracin 212, 212A, and 250A | Image harvested from NTRS | |||
5 | NACA-RM-51C21 | Effects of humidity during fabrication on some physical properties of glass-fabric unsaturated-polyester laminates | Image harvested from NTRS | |||
6 | NACA-RM-51D20 | Review of current and anticipated lubricant problems in turbojet engines | Image harvested from NTRS | |||
7 | NACA-RM-51D23 | Notes on heat-resistant materials in Britain from technical mission October 13 to November 30, 1950 | Image harvested from NTRS | |||
8 | NACA-RM-51E04 | Investigation of torsion creep-to-rupture properties of N-155 alloy | Image harvested from NTRS | |||
9 | NACA-RM-51G11 | Effective modulus in plastic buckling of high-strength aluminum-alloy sheet | Image harvested from NTRS | |||
10 | NACA-RM-51K06 | Investigation of stresses due to thermal gradients in typical aircraft structures | Image harvested from NTRS | |||
11 | NACA-RM-51K29 | Graphic Analysis of American and British Axial-Flow Turbojet Engine Performance Trends (Current and Future) | Image harvested from NTRS | |||
12 | NACA-RM-52D03 | Design of apparatus for determining heat transfer and frictional pressure drop of nitric acid flowing through a heated tube | Image harvested from NTRS | |||
13 | NACA-RM-52D11 | Supplementary bibliography of NACA reports related to instrumentation and research techniques | Image harvested from NTRS | |||
14 | NACA-RM-52F19 | Development of metal-bonding adhesive FPL-710 with improved heat-resistant properties | Image harvested from NTRS | |||
15 | NACA-RM-52I09 | A meter for timing the flow of very small volumes of a gas | Image harvested from NTRS | |||
16 | NACA-RM-52I25 | Moore, R L (Aluminum Company of America) Clark, J W (Aluminum Company of America); Torsion, compression, and bending tests of tubular sections machined from 75S-T6 rolled round rod; naca-rm-52i25; November 12, 1952 | U Cinc. has sent | |||
17 | NACA-RM-53B19 | Weight bar charts | Image harvested from NTRS | |||
18 | NACA-RM-53D14 | Effects of high degrees of biaxial stretch forming on crazing and other properties of acrylic plastic glazing | Image harvested from NTRS | |||
19 | NACA-RM-53D28 | A compilation of summaries from NACA reports on fuels research, 1945-1952 | Image harvested from NTRS | |||
20 | NACA-RM-53L22 | Additional fatigue tests on effects of design details in 355-T6 sand-cast aluminum alloy | Image harvested from NTRS | |||
21 | NACA-RM-54A04 | Effects of molecular weight on crazing and tensile properties of polymethyl methacrylate | Image harvested from NTRS | |||
22 | NACA-RM-54D01 | Development of metal-bonding adhesives with improved heat-resistant properties | Image harvested from NTRS | |||
23 | NACA-RM-54D19 | Preliminary measurements of turbulence and temperature fluctuations behind a heated grid | Image harvested from NTRS | |||
24 | NACA-RM-54F01 | Bibliography of NACA reports related to aircraft control and guidance systems January 1949 - April 1954 | Image harvested from NTRS | |||
25 | NACA-RM-54F22 | Effects of multiaxial stretching on crazing and other properties of transparent plastics | Image harvested from NTRS | |||
26 | NACA-RM-54G26 | Effects of resin coating methods and other variables on physical properties of glass-fabric reinforced polyesters | Image harvested from NTRS | |||
27 | NACA-RM-54H23 | Turbojet Propulsion-System Research and the Resulting Effects on Airplane Performance | Image harvested from NTRS | |||
28 | NACA-RM-54J27 | Some results of flight testing of ski-equipped aircraft at the Naval Air Test Center | Image harvested from NTRS | |||
29 | NACA-RM-54K24 | Description and bibliography of NACA research on wing controls : January 1946 - February 1955 | Image harvested from NTRS | |||
30 | NACA-RM-54L29 | Meteorological problems associated with commercial turbojet-aircraft operation | Image harvested from NTRS | |||
31 | NACA-RM-55F08 | Metal-bonding adhesives for high-temperature service | Image harvested from NTRS | |||
32 | NACA-RM-55I30 | Static shear strength of 2117-T4 (A17S-T4) aluminum-alloy rivets at elevated temperatures | Image harvested from NTRS | |||
33 | NACA-RM-55K16 | Application of non-afterburning turbojets to supersonic flight | Image harvested from NTRS | |||
34 | NACA-RM-56B07 | Elevated-temperature fatigue properties of two titanium alloys | Image harvested from NTRS | |||
35 | NACA-RM-56C20 | Correlation of creep-buckling tests with theory | Image harvested from NTRS | |||
36 | NACA-RM-56D27 | Stability of systems containing a heat source : the Rayleigh criterion | Image harvested from NTRS | |||
37 | NACA-RM-56I12 | A survey and evaluation of flutter research and engineering | Image harvested from NTRS | |||
38 | NACA-RM-57A30 | Problem of slip flow in aerodynamics | Image harvested from NTRS | |||
39 | NACA-RM-57B25 | Propagation of sound into a wind-created shadow zone | Image harvested from NTRS | |||
40 | NACA-RM-57E17 | Experimental investigation of creep bending and buckling of thin circular cylindrical shells | Image harvested from NTRS | |||
41 | NACA-RM-58B11 | Local isotropy in turbulent shear flow | Image harvested from NTRS | |||
42 | NACA-RM-8C29 | A restricted list of aircraft materials research projects | Image harvested from NTRS | |||
43 | NACA-RM-8I07 | Response of a Rotating Propeller to Aerodynamic Excitation | Image harvested from NTRS | |||
44 | NACA-RM-8J05 | (Author(s) Not Available); Bibliography of NACA and other reports on air inlets and internal flows; naca-rm-8j05; October 11, 1948 | Need Image | |||
45 | NACA-RM-9A05 | Determination of rate, area, and distribution of impingement of waterdrops on various airfoils from trajectories obtained on the differential analyzer | Image harvested from NTRS | |||
46 | NACA-RM-9D06 | U Cinc. has sent | ||||
47 | NACA-RM-9D13 | Summary of the availability and performance problems of high octane number fuels | Image harvested from NTRS | |||
48 | NACA-RM-A50A03 | Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds : stability and control characteristics | Image harvested from NTRS | |||
49 | NACA-RM-A50A04 | Stall Characteristics Obtained from Flight 10 of Northrop X-4 No. 2 Airplane (USAF No. 46-677) | Image harvested from NTRS | |||
50 | NACA-RM-A50A04a | Chordwise and spanwise loadings measured at a large triangular wing having an aspect ratio of 2 and a thin, subsonic-type airfoil section | Image harvested from NTRS | |||
51 | NACA-RM-A50A13 | An experimental investigation of a jet-engine nacelle in several positions on a 37.25 degree swept-back wing | Image harvested from NTRS | |||
52 | NACA-RM-A50A23 | Wind-tunnel investigation at low speed of a wing swept-back 63 degrees and twisted and cambered for a uniform load at a lift coefficient of 0.5 | Image harvested from NTRS | |||
53 | NACA-RM-A50A31a | Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness of an elevon as a longitudinal control and the effects of camber and twist on the maximum lift-drag ratio at supersonic speeds | Image harvested from NTRS | |||
54 | NACA-RM-A50B13 | Pressure coefficients at Mach numbers from 0.60 to 0.85 for a semispan wing with NACA 0012-64 section, 20-percent-chord plain aileron, and 0 degree and 45 degree sweepback | Image harvested from NTRS | |||
55 | NACA-RM-A50C13 | Preliminary investigation of the transonic characteristics of an NACA submerged inlet | Image harvested from NTRS | |||
56 | NACA-RM-A50C20 | Wind-tunnel investigation at Mach numbers of 2.0 and 2.9 of several configurations of a supersonic ram-jet test vehicle | Image harvested from NTRS | |||
57 | NACA-RM-A50C30 | Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds : additional stability and control characteristics and the aerodynamic effects of external stores and ram jets | Image harvested from NTRS | |||
58 | NACA-RM-A50D04 | Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections | Image harvested from NTRS | |||
59 | NACA-RM-A50D06 | Flight determination of the effects of rudder-pedal-force characteristics on the aiming error in azimuth of a conventional fighter airplane | Image harvested from NTRS | |||
60 | NACA-RM-A50D07 | Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds : wing and fuselage pressure distribution | Image harvested from NTRS | |||
61 | NACA-RM-A50D27 | Longitudinal-stability characteristics of the Northrop X-4 airplane (USAF No. 46-677) | Image harvested from NTRS | |||
62 | NACA-RM-A50E02 | Pressure-distribution and ram-recovery characteristics of NACA submerged inlets at high subsonic speeds | Image harvested from NTRS | |||
63 | NACA-RM-A50E09 | The effects of compressibility on the pressures on a body of revolution and on the aerodynamic characteristics of a wing-nacelle combination consisting of the body of revolution mounted on a swept-back wing | Image harvested from NTRS | |||
64 | NACA-RM-A50E10 | The transonic characteristics of a low-aspect-ratio triangular wing with a constant-chord flap as determined by wing-flow tests, including correlation with large-scale tests | Image harvested from NTRS | |||
65 | NACA-RM-A50E26 | Investigation at high subsonic speeds of methods of alleviating the adverse interference at the root of a swept-back wing | Image harvested from NTRS | |||
66 | NACA-RM-A50F06 | Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02 | Image harvested from NTRS | |||
67 | NACA-RM-A50F09 | Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effect of sideslip on aerodynamic characteristics at a Mach number of 1.4 with the wing twisted and cambered | Image harvested from NTRS | |||
68 | NACA-RM-A50F13 | An experimental investigation at large scale of an NACA submerged intake and deflector installation on the rearward portion of a fuselage | Image harvested from NTRS | |||
69 | NACA-RM-A50G06 | Low-speed investigation of a 0.16-scale model of the X-3 airplane : longitudinal characteristics | Image harvested from NTRS | |||
70 | NACA-RM-A50G10 | Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effect of Reynolds number at supersonic Mach numbers on the longitudinal characteristics of a wing twisted and cambered for uniform load | Image harvested from NTRS | |||
71 | NACA-RM-A50H02 | Effect of dihedral change on the theoretical dynamic lateral response characteristics of a low-aspect-ratio straight-wing supersonic airplane | Image harvested from NTRS | |||
72 | NACA-RM-A50H03 | Preliminary flight investigation of the wing-dropping tendency and lateral-control characteristics of a 35 degree swept-wing airplane at transonic Mach numbers | Image harvested from NTRS | |||
73 | NACA-RM-A50H09 | The use of area suction for the purpose of delaying separation of air flow at the leading edge of a 63 degree swept-back wing | Image harvested from NTRS | |||
74 | NACA-RM-A50H10 | Lateral control characteristics and dihedral effect of a wing-body combination with a variable incidence triangular wing and wing-tip ailerons at a Mach number of 1.52 | Image harvested from NTRS | |||
75 | NACA-RM-A50H17 | High-speed aerodynamic characteristics of a lateral-control model III : section characteristics, fence studies, and tabulated pressure coefficients with modified NACA 0012-64 section, 26.6-percent-chord, plain aileron, 0 and 45 degree sweepback | Image harvested from NTRS | |||
76 | NACA-RM-A50H23 | Wind-tunnel investigation of the effects of a jet engine nacelle on the aerodynamic characteristics of a 37.25 degree swept back wing at high subsonic speeds | Image harvested from NTRS | |||
77 | NACA-RM-A50H24 | U Cinc. has sent | ||||
78 | NACA-RM-A50I01 | Summary report of results obtained during demonstration tests of the Northrop X-4 airplanes | Image harvested from NTRS | |||
79 | NACA-RM-A50I11 | Wind-tunnel investigation of a 1/6-scale model of the Bumblebee XPM missile at high subsonic speeds | Image harvested from NTRS | |||
80 | NACA-RM-A50I14 | Wind-tunnel investigation at low speed of a wing swept back 63 degrees and twisted and cambered for uniform load at a lift coefficient of 0.5 and with a thickened tip section | Image harvested from NTRS | |||
81 | NACA-RM-A50I14a | Investigation of the downwash and wake behind a triangular wing of aspect ratio 4 at subsonic and supersonic Mach numbers | Image harvested from NTRS | |||
82 | NACA-RM-A50I27 | Flight determined buffet boundaries of ten airplanes and comparisons with five buffeting criteria | Image harvested from NTRS | |||
83 | NACA-RM-A50J09 | Lift and moment characteristics at subsonic Mach numbers of four 10-percent-thick airfoil sections of varying trailing-edge thickness | Image harvested from NTRS | |||
84 | NACA-RM-A50J09a | Preliminary flight investigation of the dynamic longitudinal-stability characteristics of a 35 degree swept-wing airplane | Image harvested from NTRS | |||
85 | NACA-RM-A50J09b | Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - trailing-edge flaps deflected | Image harvested from NTRS | |||
86 | NACA-RM-A50J17 | A comparison of the experimental and theoretical loading over triangular wings at supersonic speeds | Image harvested from NTRS | |||
87 | NACA-RM-A50J24 | The effects of camber and twist on the aerodynamic loading and stalling characteristics of a large-scale 45 degree swept-back wing | Image harvested from NTRS | |||
88 | NACA-RM-A50J26 | Experimental damping in pitch of 45 degree triangular wings | Image harvested from NTRS | |||
89 | NACA-RM-A50J26a | Aerodynamic characteristics including pressure distribution of a fuselage and three combinations of the fuselage with swept-back wings at high subsonic speeds | Image harvested from NTRS | |||
90 | NACA-RM-A50K06 | The effects of boundary-layer control on the longitudinal characteristics of a swept-back wing using suction through streamwise slots in the outboard portion of the wing | Image harvested from NTRS | |||
91 | NACA-RM-A50K07 | Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness at supersonic speeds of a 30-percent chord, 50-percent semispan elevon as a lateral control device | Image harvested from NTRS | |||
92 | NACA-RM-A50K10 | Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept, tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - leading-edge flaps deflected | Image harvested from NTRS | |||
93 | NACA-RM-A50K15 | The effects of centrally mounted wing-tip tanks on the subsonic aerodynamic characteristics of a wing of aspect ratio 10 with 35 degrees of sweepback | Image harvested from NTRS | |||
94 | NACA-RM-A50K20 | Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 2 with NACA 0008-63 section | Image harvested from NTRS | |||
95 | NACA-RM-A50K21 | Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 2 with NACA 0005-63 section | Image harvested from NTRS | |||
96 | NACA-RM-A50K24 | Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 4 with NACA 0005-63 section | Image harvested from NTRS | |||
97 | NACA-RM-A50K24a | Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 2 with NACA 0003-63 section | Image harvested from NTRS | |||
98 | NACA-RM-A50K24b | Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 4 with NACA 0005-63 thickness distribution, cambered and twisted for trapezoidal span load distribution | Image harvested from NTRS | |||
99 | NACA-RM-A50K27 | The effects of Mach number and Reynolds number on the aerodynamic characteristics of several 12-percent-thick wings having 35 degrees of sweepback and various amounts of camber | Image harvested from NTRS | |||
100 | NACA-RM-A50K27a | Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds: Triangular Wing of Aspect Ratio 2 with NACA 0005-63 Thickness Distribution, Cambered and Twisted for a Trapezoidal Span Load Distribution | Image harvested from NTRS |