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- Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degree Sweptback Wing at Reynolds Numbers to 8,000,000
- Method of Characteristics for Three-Dimensional Axially Symmetrical Supersonic Flows
- Investigation of the dynamic response of airplane wings to gusts
- An Investigation at Low Speed of a Large-Scale Triangular Wing of Aspect Ratio Two 1: Characteristics of a Wing Having a Double-Wedge Airfoil Section With Maximum Thickness at 20-Percent Chord
- Theoretical study of air forces on an oscillating or steady thin wing in a supersonic main stream
- A unified theory of plastic buckling of columns and plates
- Considerations of the Total Drag of Supersonic Airfoil Sections
- Airfoil in Sinusoidal Motion in a Pulsating Stream
- The 1350 F stress-rupture properties of two wrought alloys and three cast alloys
- Planing of Watercraft
- Flight Measurements of Buffeting Tail Loads
- An experimental investigation of the design variables for NACA submerged duct entrances
- Air-flow surveys in the vicinity of representative NACA 1-series cowlings
- Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps
- Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps
- An Investigation of the Wing and the Wing-Fuselage Combination of a Full-Scale Model of the Republic XP-91 Airplane in the Ames 40-by 80-Foot Wing Tunnel
- Preliminary Results of British Nene II Engine Altitude-Chamber Performance Investigation. I - Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle, 1, Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle
- Calculations of the Dynamic Stress of Several Airplane Wings in Various Gusts
- Performance of J-33-A-21 Turbojet-Engine Compressor I - Over-All Performance Characteristics at Equivalent Impeller Speeds from 6000 to 13,400 RPM
- Comparison of Drop and Wind-Tunnel Experiments on Bomb Drag at High Subsonic Speeds
- The Influence of the Diameter Ratio on the Characteristics Diagram of the Axial Compressor
- Measurements on Compressor-Blade Lattices
- Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine, Part 5, Performance and Windmilling Drag Characteristics
- Performance of Compressor of XJ-41-V Turbojet Engine VI - Analysis of Compressor Flow Choking, 6, Analysis of Compressor Flow Choking
- Ground Tests of a Radial Air-Cooled Engine to Correct a Poor Circumferential Pressure-Recovery Distribution
- Simulated Altitude Performance of Combustor of Westinghouse 19XB-1 Jet-Propulsion Engine
- Simulated Altitude Performance of Combustors for the Westinghouse 24C Jet Engine I-24C-2 Combustor
- Effect of Distribution of Basket-Hole Area on Simulated Altitude Performance of 25 1/2-Inch-Diameter Annular-Type Turbojet Combustor
- Performance of Compressor of XJ-41-V Turbojet Engine, 4, Performance Analysis Over Range of Compressor Speeds from 5000 to 10,000 RPM
- Performance of J33-A-23 Turbojet-Engine Compressor, Part 1, Over-All Performance Characteristics of Compressor with 17-Blade Impeller
- Performance of J33-A-23 Turbojet-Engine Compressor, II, Over-All Performance Characteristics of Compressor with 34-Blade Impeller at Equivalent Impeller Speeds from 6000 to 11.750 RPM
- Theoretical Comparison of Several Methods of Thrust Augmentation for Turbojet Engines
- Performance of J-33-A-21 and J-33-A-23 Compressors with and without Water Injection
- Tank Tests of a Powered Model of a Compression Plane, NACA Model 171A-2
- Natural icing of an axial-flow turbojet engine in flight for a single icing condition
- Investigation of Effectiveness of Air-Heating a Hollow Steel Propeller for Protection Against Icing 1: Unpartitioned Blades
- Investigation of Effectiveness of Air-Heating a Hollow Steel Propeller for Protection Against Icing. 2: 50% Impartitioned Blades
- Investigation of Effectiveness of Air-Heating a Hollow Steel Propeller for Protection Against Icing. 3: 25% Partitioned Blades
- An investigation of fretting corrosion under several conditions of oxidation
- Stability and control characteristics at low speed of an airplane model having a 38.7 degree sweptback wing with aspect ratio 4.51, taper ratio 0.54, and conventional tail surfaces
- Flight determination of wing and tail loads on a fighter-type airplane by means of strain-gage measurements
- Flight measurements of the longitudinal stability, stalling, and lift characteristics of an airplane having a 35 degrees sweptback wing without slots and with 40-percent-span slots and a comparison with wind-tunnel data
- Flight measurements of the stability, control, and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-span slots and a comparison with wind-tunnel data
- Bearing tests of 14S sheet and plate
- Flow of a compressible fluid past a symmetrical airfoil in a wind tunnel and in free air
- An Investigation of Aircraft Heaters 26: Development of a Sensitive Plated-Type Thermopile for Measuring Radiation
- Investigation of a 1/7-scale powered model of a twin-boom airplane and a comparison of its stability, control, and performance with those of a similar all-wing airplane
- Investigation of the validity of an ideal theory of elasto-plasticity for wrought aluminum alloys
- Investigation of the variation of maximum lift for a pitching airplane model and comparison with flight results
- Characteristics of thin triangular wings with constant-chord partial-span control surfaces at supersonic speeds