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- An Investigation of the Hydrodynamic Characteristics of a Jet-Powered Dynamic Model of the DR 56 Flying Boat: TED No. NACA DE 328
- An Investigation of Flow Characteristics at Mach Number 4.04 Over 6- and 9-Percent-Thick Symmetrical Circular-Arc Airfoils Having 30-Percent-Chord Trailing-Edge Flaps
- 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
- An Analytic Determination of the Flow Behind a Symmetrical Curved Shock in a Uniform Stream
- Free-Flight Investigation of the Longitudinal Stability and Control of a Rocket-Propelled Missile Model Having Cruciform, Triangular, Interdigitated Wings and Tails
- Horizontal-Tail Effectiveness and Downwash Surveys for Two 47.7 Degree Sweptback Wing-Fuselage Combinations With Aspect Ratios of 5.1 and 6.0 at a Reynolds Number of 6.0 X 10(Exp 6)
- Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Measurements of the Distribution of the Aerodynamic Load Among the Wing, Fuselage, and Horizontal Tail at Mach Numbers Up to 0.87
- Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Static Longitudinal Stability and Control Characteristics at Mach Numbers Up to 0.87
- Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Dynamic Lateral Stability
- Investigation at Supersonic Speeds of Some of the Factors Affecting the Flow Over a Rectangular Wing With Symmetrical Circular-Arc Section and 30-Percent-Chord Trailing-Edge Flap
- An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degree Sweepback: Force Characteristics of the Complete Configuration and Its Various Components at Mach Numbers of 1.40 and 1.59
- Experimental investigation of tail-pipe-burner design variables
- Investigations on Wings With and Without Sweepback at High Subsonic Speeds
- On the Turbulent Friction Layer for Rising Pressure
- On the recording of turbulent longitudinal and transverse fluctuations
- Flight-Determination of the Low-Lift Drag and Longitudinal Stability of a 1/10-Scale Rocket-Powered Model of the Douglas XF4D-1 Airplane at Mach Numbers from 0.7
- Preliminary Transient Performance Data for Afterburner Operation of Westinghouse Electronic Power Regulator on XJ34-WE-32 Turbojet Engine in Altitude Wind Tunnel
- On Ionization and Luminescence in Flames
- Deplacement Effect of the Laminar Boundary Layer and the Pressure Drag
- Supplementary Ditching Investigation of a 1/18-Scale Model of the North American B-45 Airplane
- A Thermodynamic Study of the Turbine-Propeller Engine
- Yawed-Landing Investigation of a Model of the Convair Y2-2 Airplane, TED No. NACA DE 363
- On Motion of Fluid in Boundary Layer Near Line of Intersection of Two Planes
- Preliminary Results of a Flight Investigation of 1/6-Scale Rocket-Powered Models of the Bell MX-776 to Determine Aileron Rolling Effectiveness and Total Drag
- Investigation of Turbulent Flow in a Two-Dimensional Channel
- The Design of Variable Mach Number Asymmetric Super-Sonic Nozzles by Two Procedures Employing Inclined and Curved Sonic Lines
- Effect of Angle of Incidence of Second-Stage Vane Assembly on Third-Stage Compressor-Blade Vibration and Engine Performance
- Annual Report of the National Advisory Committee for Aeronautics (38th). Administrative Report Including Technical Report Nos. 1059 to 1110
- Annual Report of the National Advisory Committee for Aeronautics (36th). Administrative Report Including Technical Report Nos. 951 to 1002
- Annual Report of the National Advisory Committee for Aeronautics (34th). Administrative Report Including Technical Report Nos. 892 to 921
- Annual Report of the National Advisory Committee for Aeronautics (35th). Administrative Report Including Technical Report Nos. 922 to 950
- Ditching Investigation of a 1/14-Scale Model of the XC-123 Airplane
- Factors Affecting the Starting Characteristics of Gas-Turbine Engines
- NACA Conference on Aircraft Structures
- Coolant-Flow Calibrations of Three Simulated Porous Gas-Turbine Blades
- Control Performance of General Electric Fuel and Torque Regulator Operating on T31-3 Turbine-Propeller Engine in Sea-Level Test Stand
- Altitude Performance of J35-A-17 Turbojet Engine in an Altitude Chamber
- Low-Lift Drag and Duct Pressure Recovery of a 1/8.25-Scale Model of the Consolidated Vultee XF-92 Airplane at Mach Numbers from 0.7 to 1.4
- Low-Speed Investigation of a Semisubmerged Air Scoop With and Without Boundary-Layer Suction
- An Investigation of the Aerodynamic Characteristics in Pitch of an XB-52 Airplane Model in a High-Speed Wind Tunnel
- An Investigation of the Drag and Pressure Recovery of a Submerged Inlet and a Nose Inlet in the Transonic Flight Range With Free-Fall Models
- Investigation of Turbine-Outlet Temperature Distribution of XJ34-WE-32 Turbojet Engine
- Investigation of the Low-Speed Stability and Control Characteristics of a 1/10-Scale Model of the Douglas XF4D-1 Airplane in the Langley Free-Flight Tunnel TED No. NACA DE 349
- Aerodynamic Characteristics of a Flying-Boat Hull Having a Length-Beam Ratio of 15, TED No. NACA 2206
- Aerodynamic Characteristics of Bodies at Supersonic Speeds: A Collection of Three Papers
- Supplementary Free-Spinning-Tunnel Investigation of a 1/30-Scale Model of the Grumman XF10F-1 Airplane in the Swept-Wing Configuration with Slats Extended
- Flight Determination of the Drag and Longitudinal Stability and Control Characteristics of a Rocket-Powered Model of a 60 Degrees Delta-Wing Airplane From Mach Numbers 0.75 to 1.70
- Review of the Maximum-Lift Characteristics of Thin and Swept Wings
- Preliminary Experimental Investigation of Flutter Characteristics of M and W Wings
- Preliminary Investigation of a Supersonic Scoop Inlet Derived From a Conical-Spike Nose Inlet