Browse TRAIL Inventories

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


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