Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
14045 results returnedSearch results
- 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
- Preliminary Investigation of the Effects of Rectangular Vortex Generators on the Performance of a Short 1.9:1 Straight-Wall Annular Diffuser
- Preliminary Investigation of the Transfer of Heat From a Flat Plate at a Mach Number of 1.5
- Application of X-Ray Absorption to Measurement of Small Air-Density Gradients
- Transonic-Wing Investigation in the Langley 8-Foot High-Speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1.2: Analysis of Pressure Distribution of Wing-Fuselage Configuration Having a Wing of 45 Degrees Sweptback, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section
- Recent Experimental Flutter Studies
- Resistance of Various Materials to Attack by Molten Bismuth-Lead Eutectic at Elevated Temperatures
- Rolling Effectiveness of All-Movable Wings at Small Angles of Incidence at Mach Numbers From 0.6 to 1.6
- Pressure Pulsations on Rigid Airfoils at Transonic Speeds
- Some Effects of Spanwise Aileron Location and Wing Structural Rigidity on the Rolling Effectiveness of 0.3-Chord Flap-Type Ailerons on a Tapered Wing Having 63 Degrees Sweepback at the Leading Edge and Naca 64A005 Airfoil Sections
- The Use of Two-Dimensional Section Data to Estimate the Low-Speed Wing Lift Coefficient at Which Section Stall First Appears on a Swept Wing
- Dynamic Stability and Control Characteristics of a Delta-Wing Vertically Rising Airplane Model in Take-Offs, Landings, and Hovering Flight
- A Wind-Tunnel Investigation of the Static Stability Characteristics of a 1/8-Scale Ejectable Pilot-Seat Combination at a Mach Number of 0.8
- The Effect of Raking the Aileron Tips on the Lateral-Control and Hinge-Moment Characteristics of a 20-Percent-Chord Partial-Span Outboard Aileron on a Wing With Leading-Edge Swept Back 51.3 Degrees
- Elevated Temperature Properties of Titanium Carbide Base Ceramals Containing Nickel or Iron
- Effects of Propeller-Shank Geometry and Propeller-Spinner-Juncture Configuration on Characteristics of an NACA 1-Series Cowling-Spinner Combination With an Eight-Blade Dual-Rotation Propeller
- Effect of Section Thickness and Trailing-Edge Radius on the Performance of NACA 65-Series Compressor Blades in Cascade at Low Speeds
- Effect of the Proximity of the Ground on the Stability and Control Characteristics of a Vertically Rising Airplane Model in the Hovering Condition
- Effect of Formation Position on Load Factors Obtained on F2H Airplanes
- Determination and Use of the Local Recovery Factor for Calculating the Effectiveness Gas Temperature for Turbine Blades
- Division of Load Among the Wing, Fuselage, and Tail of Aircraft
- Charts Giving Critical Compressive Stress of Continuous Flat Sheet Divided Into Parallelogram-Shaped Panels
- Comparison of High-Speed Operating Characteristics of Size 215 Cylindrical-Roller Bearings as Determined in Turbojet Engine and in Laboratory Test Rig
- Comparison of Semispan and Full-Span Tests of a 47.5 Degrees Sweptback Wing With Symmetrical Circular-Arc Sections and Having Drooped-Nose Flaps, Trailing-Edge Flaps, and Ailerons
- Derivation of the Equations of Motion of a Symmetrical Wing-Tip-Coupled Airplane Configuration With Rotational Freedom at the Junctures
- Characteristics of a Wedge With Various Holder Configurations for Static-Pressure Measurements in Subsonic Gas Streams
- Damping in Roll of Straight and 45 Degree Swept Wings of Various Taper Ratios Determined at High Subsonic, Transonic, and Supersonic Speeds With Rocket-Powered Models
- Damping in Roll of Rocket-Powered Test Vehicles Having Swept, Tapered Wings of Low Aspect Ratio
- Calculated Aerodynamic Loadings of M, W, and Delta Wings in Incompressible Flow
- Additional Studies of the Stability and Controllability of an Unswept-Wing Vertically Rising Airplane Model in Hovering Flight Including Studies of Various Tethered Landing Techniques
- Altitude-Wind-Tunnel Investigation of Performance Characteristics of a J47D Prototype (RX1-1) Turbojet Engine With Fixed-Area Exhaust Nozzle
- Flight Investigation at Subsonic, Transonic, and Supersonic Velocities of the Hinge-Moment Characteristics, Lateral-Control Effectiveness, and Wing Damping in Roll of a 60 Degrees Sweptback Delta Wing With Half-Delta Tip Ailerons (Revised)
- Flight Investigation of the Longitudinal Stability and Control Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Up to 0.89
- Low-Speed Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 From Pressure Distributions and Force Tests at Reynolds Numbers From 1,500,000 to 4,800,000
- An Investigation of the Aerodynamic Characteristics of a Series of Cone-Cylinder Configurations at a Mach Number of 6.86
- Investigation of the Effect of a Nacelle at Various Chordwise and Vertical Positions on the Aerodynamic Characteristics at High Subsonic Speeds of a 45 Degrees Sweptback Wing With and Without a Fuselage