Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
14045 results returnedSearch results
- Observations on an aileron-flutter instability encountered on a 45 degree swept-back wing in transonic and supersonic flight
- Preliminary Tests to Determine the Maximum Lift of Wings at Supersonic Speeds
- Wind-Tunnel Investigation of Bomb-Bay Configurations Intended to Minimize the Tumbling of Light-Weight Bombs
- Six-Component Measurements on a Straight and a 35 Degree Swept-Back Trapezoidal Wing With and Without Split Flaps
- Practical Possibilities of High-Altitude Flight with Exhaust-Gas Turbines in Connection with Spark Ignition Engines Comparative Thermodynamic and Flight Mechanical Investigations
- Performance Charts for a Turbojet System
- Performance of a Mixed-Flow Impeller in Combination with Semivaneless Diffuser
- Some Tests and Calculations Pertaining to the Dive Path and to Wing and Tail Loads in the Accident to Eastern Airlines C54B Airplane, NC-88814, Near Bainbridge, Maryland, May 30, 1947
- Stability of Plates and Shells Beyond the Proportional Limit
- The Separation of Flow Due to Compressibility Shock
- Simulated Altitude Investigation of Stewart-Warner Model 906-B Combustion Heater
- Systematic Wind-Tunnel Measurements on Missiles
- The Calculation of Compressible Flows with Local Regions of Supersonic Velocity
- A Time History of Control Operation of a C-54 Airplane in Blind Landing Approaches
- Results of Flight Test of an Automatically Stabilized Model C (Swept Back) Four-Wing Tiamat
- Supersonic Wave Drag of Sweptback Tapered Wings at Zero Lift
- Scale Effect and Optimum Relations for Sea Surface Planning
- Theoretical Evaluation of Methods of Cooling the Blades of Gas Turbines
- Vibration Survey of Blades in 19XB Axial-Flow Compressor 2: Dynamic Investigation
- An Analysis of the Full-Floating Journal Bearing
- Wind-Tunnel Tests of a 1/8-Scale Powered Model of the XTB3F-1 Airplane, TED No. NACA 2382
- A Theory of Unstaggered Airfoil Cascades in Compressible Flow
- A Theory of Unstaggered Airfoil Cascades in Compressible Flow
- Tests of a Horizontal-Tail Model through the Transonic Speed Range by the NACA Wing-Flow Method
- Pressure-Distribution Measurements on Unyawed Swept-Back Wings
- Tests of Cascades of Airfoils for Retarded Flow
- Russian Laminar Flow Airfoils 3rd Part: Measurements on the Profile No. 2315 BIS with Ava-Nose Flap
- Some Aerodynamic Relations for an Airfoil in Oblique Flow
- Temperatures and Stresses on Hollow Blades For Gas Turbines
- Test Report on Measurements on a Series of Tapered Wings of Small Aspect Ratio (Trapezoidal Wing with Fuselage)
- Infinitesimal Conical Supersonic Flow
- On Combustion in a Turbulent Flow
- On the Vortex Sound from Rotating Rods
- On the Application of the Energy Method to Stability Problems
- On the Theory of the Unsteady Motion of an Airfoil
- Preliminary Report on the Fundamentals of the Control of Turbine-Propeller Jet Power Plant
- Investigation of the Operating Properties of the Leakage Current Anemometer
- The Effect of Turbulence on the Flame Velocity in Gas Mixtures
- Equations for Adiabatic but Rotational Steady Gas Flows Without Friction
- Force and Pressure-Distribution Measurements on a Rectangular Wing With Double-Hinged Nose
- Gas-Dynamic Investigations of the Pulse-Jet Tube, Parts 1 and 2
- [Memorandums on the Subject of D-558 Airplane]
- High-Speed Measurements on a Swept-Back Wing (Sweepback Angle phi = 35 Deg)
- The Load Distribution in Bolted or Riveted Joints in Light-Alloy Structures
- Effect of Various Methods of Boundary-Layer Control on Performance of V-1710-93 Engine-Stage Supercharger
- Effect of Air-Flow Distribution and Total-Pressure Loss on Performance of One-Sixth Segment of Turbojet Combuster
- Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms: September 5, 1946 to September 10, 1946 at Orlando, Florida
- The Effectiveness at High Speeds of a 20-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil Section
- Effect of Engine Skew on Directional and Lateral Control Characteristics of Single-Engine Airplanes
- Drag Corrections in High-Speed Wind Tunnels