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- Note on similarity conditions for flows with heat transfer
- Simulated-Altitude Investigations of Performance of Tubular Aircraft Oil Coolers
- Effect of Hydrocarbon Type and Chain Length on Uniform Flame Movement in Quiescent Fuel-Air Mixtures
- An Investigation of Mechanical Properties of Honeycomb Structures Made of Resin-Impregnated Paper
- Stress Distribution in a Beam of Orthotropic Material Subjected to a Concentrated Load
- Wind-tunnel investigation of seven thin NACA airfoil sections to determine optimum double-slotted-flap configurations
- Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50- airfoil chord plain sealed flaps
- Effect of Variables in Welding Technique on the Strength of Direct-Current Metal-Arc-Welded Joints in Aircraft Steel 2 - Repeated-Stress Tests of Joints in SAE 4130 Seamless Steel Tubing
- Preliminary Results of NACA Transonic Flights of the XS-1 Airplane With a 10-Percent-Thick Wing and 8-Percent-Thick Horizontal Tail
- Flight and Wind-Tunnel Investigation to Determine the Aileron-Vibration Characteristics of 1/4-Scale Wing Panels of the Douglas D-558-2 Research Airplane
- Flight Characteristics at Low Speed of Delta-Wing Models
- Preliminary Investigation of a Ceramic Lining for a Combustion Chamber for Gas-Turbine Use
- A Summary and Analysis of Wind-Tunnel Data on the Lift and Hinge-Moment Characteristics of Control Surfaces Up to a Mach Number of 0.90
- Two-Dimensional Wind-Tunnel Investigation at High Reynolds Numbers of an NACA 65A006 Airfoil With High-Lift Devices
- Pressure Distributions Over a Wing-Fuselage Model at Mach Numbers of 0.4 to 0.99 and at 1.2
- Wind-Tunnel Investigation of a Wing-Fuselage Combination With External Stores
- Wind-Tunnel Investigation at a Mach Number of 1.53 of an Airplane With a Triangular Wing
- A Wind-Tunnel Investigation at Low Speed of Various Lateral Controls on a 45 Degree Swept-Back Wing
- Wind-Tunnel Investigation of the Low-Speed Stability and Control Characteristics of a Model With a Sweptback Vee Tail and a Sweptback Wing
- Yaw Characteristics of a 52 Degree Sweptback Wing of NACA 64(Sub 1)-112 Section With a Fuselage and With Leading-Edge and Split Flaps at Reynolds Numbers From 1.93 X 10(Exp 6) to 6.00 X 10(Exp 6)
- Wind-Tunnel Investigation of the Stability of Jettisoned Nose Sections of the D-558 Airplane: Phases 1 and 2
- Drag Measurements in Flight on the 10-Percent-Thick and 8-Percent-Thick Wing X-1 Airplanes
- Aerodynamic Characteristics of Several NACA Airfoil Sections at Seven Reynolds Numbers From 0.7 X 10(Exp 6) to 9.0 X 10(Exp 6)
- Comparison of Hovering Performance of Helicopters Powered by Jet-Propulsion and Reciprocating Engines
- Cyclic Engine Test of Cast Vitallium Turbine Buckets - 1
- Aerodynamic Characteristics of Flying-Boat Hulls Having Length-Beam Ratios of 20 and 30
- An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence
- Longitudinal-Stability Investigation of High-Lift and Stall-Control Devices on a 52 Degree Sweptback Wing With and Without Fuselage and Horizontal Tail at a Reynolds Number of 6.8 X 10 (Exp 6)
- Investigation of Effects of Several Fuel-Injection Locations on Operational Performance of a 20-Inch Ram Jet
- An Investigation of Aileron Oscillations at Transonic Speeds on NACA 23012 and NACA 65-212 Airfoils by the Wing-Flow Method
- Helicopter Stability
- Longitudinal Stability and Control Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds From Tests by the NACA Wing-Flow Method
- Additional Results in a Free-Flight Investigation of Control Effectiveness of Full-Span, 0.2-Chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Aspect Ratio, Taper, and Section Thickness Ratio
- High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane Basic Longitudinal Stability of the D-558-1
- High-Speed Wind-Tunnel Tests of a Model Pursuit Airplane and Correlation With Flight-Test Results
- Flight Tests to Determine the Effect of Airfoil Section Profile and Thickness Ratio on the Zero-Lift Drag of Low-Aspect-Ratio Wings at Supersonic Speeds
- Initial Flight Test of the NACA FR-1-A, a Low-Acceleration Rocket-Propelled Vehicle for Transonic Flutter Research
- Initial Flight Tests of the NACA FR-2, a High-Velocity Rocket-Propelled Vehicle for Transonic Flutter Research
- High-Speed Wind-Tunnel Investigation of a Flying-Boat Hull With High Length-Beam Ratio
- High-speed wind-tunnel tests of a 1/16-scale model of the D-558 research airplane-dynamic pressure and comparison of point and effective downwash at the tail of the D-558-1
- Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Lark Pilotless-Aircraft Configuration
- Flutter Investigation in the Transonic Range of Six Airfoils Attached to Three Freely Falling Bodies
- Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-Foot Pressure Wind Tunnel 3: The Effectiveness of a Constant-Chord Aileron
- Effect of a pilot's canopy on the drag of an NACA RM-2 drag research model in flight at transonic and supersonic speeds
- Correlation of wind-tunnel and flight determinations of the buffet speed of an airplane equipped with external stores
- Performance of Experimental Turbojet-Engine Combustor 1: Performance of a One-Eighth Segment of an Experimental Turbojet-Engine Combustor
- Static tests of a shrouded and an unshrouded propeller
- Pressure distribution over a sharp-nose body of revolution at transonic speeds by the NACA wing-flow method
- Measurements of the wing and tail loads during the acceptance tests of Bell XS-1 research airplane
- The NACA 2000-horsepower propeller dynamometer and tests at high speed of an NACA 10-(3)(08)-03 two-blade propeller