Browse TRAIL Inventories

Experimental Investigation of Axial-Flow Compressor Stator Blades Designed to Obtain High Turning Angles by Means of Boundary-Layer Suction

Use of Fences to Increase Uniformity of Boundary Layer on Side Walls of Supersonic Wind Tunnels

Radiant Heat Transfer From Flames in a Single Tubular Turbojet Combustor

Some Dynamic Characteristics of a Turbojet Engine for Large Accelerations

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

Friction and Wear

The Excitation of Unstable Perturbations in a Laminar Friction Layer

Wind-Tunnel Corrections at High Subsonic Speeds Particularly for an Enclosed Circular Tunnel

Calculation of the Lateral-Dynamic Stability of Aircraft

Comparison of Turbojet-Engine Altitude Performance Characteristics and Ignition Limits With MIL-F-5624A Fuel, Grades JP-3 and JP-4

Investigations of the Boundary-Layer Control on a Full Scale Swept Wing With Air Bled Off From the Turbojet

Development of a Laminar Boundary Layer Behind a Suction Point

Generalized Theory for Seaplane Impact

Theory and Procedure for Determining Loads and Motions in Chine-Immersed Hydrodynamic Impacts of Prismatic Bodies

Concerning the Flow About Ring-Shaped Cowlings of Finite Thickness: Part 1

Concerning the Flow About Ring-Shaped Cowlings Part 8: Further Measurements on Annular Profiles

On a Solution of the Nonlinear Differential Equation for Transonic Flow Past a Wave-Shaped Wall

Extension to the Cases of Two Dimensional and Spherically Symmetric Flows of Two Particular Solutions to the Equations of Motion Governing Unsteady Flow in a Gas

The Structure of Turbulence in Fully Developed Pipe Flow

On the Development of Turbulent Wakes From Vortex Streets

An Experimental Investigation of Transonic Flow Past Two-Dimensional Wedge and Circular-Arc Sections Using a Mach-Zehnder Interferometer

Relation Between Roughness of Interface and Adherence of Porcelain Enamel to Steel

Experimental Determination of the Effect of Horizontal-Tail Size, Tail Length, and Vertical Location on Low-Speed Static Longitudinal Stability and Damping Pitch of a Model Having 45 Degree Sweptback Wing and Tail Surfaces

An Iterative Transformation Procedure for Numerical Solution of Flutter and Similar Characteristics-Value Problems


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