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Spreading of Exhaust Jet From 16 Inch Ream Jet at Mach Number 2.0

A Meter for Timing the Flow of Very Small Volumes of a Gas

A Study of the Application of Power-Spectral Methods of Generalized Harmonic Analysis to Gust Loads on Airplanes

Effect of Geometry on Secondary Flows in Blade Rows

Chordwise and Compressibility Corrections to Slender-Wing Theory

Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds: Plane Triangular Wing of Aspect Ratio 3 With Air-to-Air Missile Models Mounted Externally

Method of Estimating the Stick-Fixed Longitudinal Stability of Wing-Fuselage Configurations Having Unswept or Swept Wings

Method and Graphs for the Evaluation of Air-Induction Systems

A Study of Second-Order Supersonic Flow Theory

An Investigation at Mach Numbers 2.98 and 2.18 of Axially Symmetric Free-Jet Diffusion with a Ram-Jet Engine

Some Wind-Tunnel Results of an Investigation of the Flutter of Sweptback- and Triangular-Wing Models at Mach Number 1.3

Use of Choked Nozzle Technique and Exhaust Jet Diffuser for Extending Operable Range of Jet-Engine Research Facilities

A Study of the Use of Freon-12 as a Wind-Tunnel Testing Medium at Low Supersonic Mach Numbers

Low-Speed Lateral-Control Investigation of a Flap-Type Spoiler Aileron With and Without a Deflector and Slot on a 6-Percent-Thick, Tapered, 45 Degree Sweptback Wing of Aspect Ratio 4

An Application of the Rocket-Propelled-Model Technique to the Investigation of Low-Lift Buffeting and the Results of Preliminary Tests

Effects of Some Primary Variables of Rectangular Vortex Generators on the Static-Pressure Rise Through a Short Diffuser

Supplementary Free-Spinning-Tunnel Investigation of a 1/20-Scale Model of the McDonnell F2H-3 Airplane with External Stores Installed: TED No. NACA DE 2393

Hinge-Moment and Other Aerodynamic Characteristics at Transonic Speeds of a Quarter-Span Spoiler on a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3

Investigation of an NACA Submerged Inlet at Mach Numbers from 1.17 to 1.99

Observations of Unsteady Flow Phenomena for an Inclined Body Fitted with Stabilizing Fins

Tests at Mach Number 1.62 of a Series of Missile Configurations Having Tandem Cruciform Lifting Surfaces

The Forces and Pressure Distribution at Subsonic Speeds on a Cambered and Twisted Wing Having 45 Degrees of Sweepback and Aspect Ratio of 3 and a Taper Ratio of 0.5

Small-Scale Transonic Investigation of the Effects of Full-Span and Partial-Leading-Edge Flaps on the Aerodynamic Characteristics of a 50 Degree 38 Foot Sweptback Wing of Aspect Ratio 2.98

On the Application of Transonic Similarity Rules to Wings of Finite Span

An Investigation at Mach Numbers of 1.62 and 1.93 of the Lift Effectiveness and Integrated Downwash Characteristics of Several In-Line Missile Configurations Having Equal-Span Wings and Tails

Control Hinge-Moment and Effectiveness Characteristics of a 60 Degree Half-Delta Tip Control on a 60 Degree Delta Wing at Mach Numbers of 1.41 and 1.96

Downwash and Sidewash Fields Behind Cruciform Wings

Preliminary Investigation of Cyclic De-Icing of an Airfoil Using an External Electric Heater

Preliminary Results of Cyclical De-Icing of a Gas-Heated Airfoil

First Landing of Bell X-2 Research Airplane

Total-Pressure-Recovery Characteristics of a Model of the McDonnell XF3H-1 Inlets and Forebody in a Free Jet at a Mach Number of 1.55

Wind-Tunnel Investigation of the Aerodynamic Characteristics of a 0.07-Scale Model of the North American MX-770 Missile

A Wind-Tunnel Investigation of the Stability of the Antisubmarine Rocket Mk 1 Mod 0

An Investigation Utilizing an Electrical Analogue of Cyclic Deicing of a Hollow Steel Propeller with an External Blade Shoe

Impingement of Cloud Droplets on a Cylinder and Procedure for Measuring Liquid-Water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method

Investigations of Air-Cooled Turbine Rotors for Turbojet Engines 1: Experimental Disk Temperature Distribution in Modified J33 Split-Disk Rotor at Speeds up to 6000 RPM

Rocket-Model Investigation of the Rolling Effectiveness of a Fighter-Type Wing-Control Configuration at Mach Numbers From

Experimental Study of Isothermal Wake-Flow Characteristics of Various Flame-Holder Shapes

Empirical Cooling Correlation for an Experimental Afterburner With an Annular Cooling Passage

Cooling Characteristics of an Experimental Tail-Pipe Burner With an Annular Cooling-Air Passage

Analysis of a Pneumatic Probe for Measuring Exhaust-Gas Temperatures with Some Preliminary Experimental Results

Measurements of Pressure Drop with No Heat Addition on Mockup Segments of the General Electric Air-Cooled Aircraft Reactor

Method for Estimating Pitching-Moment Interference of Wing-Body Combinations at Supersonic Speed

A Method for Estimating the Components of Lift of Wing-Body Combinations at Supersonic Speeds

Radiant Heat Transfer From Flames in a Single Tubular Turbojet Combuctor

Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems-Effect of Method of Positioning the Radar Antenna on the Speed of Response

General Correlation of Temperature Profiles Downstream of a Heated Air Jet Directed at Various Angles to Air Stream

Investigation at Mach Number 1.91 of Spreading Characteristics of Jet Expanding From Choked Nozzles

Effect of Design Changes of Operating Conditions on Combustion and Operational Performance of a 28-Inch Diameter Ram-Jet Engine

Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle


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