Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
7169 results returnedSearch results
- Investigation of a Tilting-Wing Vertical-Take-Off-and-Landing Jet Airplane Model in Hovering and Transition Flight
- Investigation of a High-Flow Transonic-Compressor Inlet Stage Having a Hub-Tip Radius of 0.35
- Fatigue Behavior of Aircraft Structural Beams
- Relationship of Metal Surfaces to Heat-Aging Properties of Adhesive Bonds
- A Low-Speed Experimental Investigation of the Effect of a Sandpaper Type of Roughness on Boundary-Layer Transition
- Aerodynamic Effects Caused by Icing of an Unswept NACA 65A004 Airfoil
- Acoustic, thrust, and drag characteristics of several full-scale noise suppressors for turbojet engines
- Accelerations in Transport-Airplane Crashes
- Studies of OH, CO, CH, and C₂ Radiation From Laminar and Turbulent Propane-Air and Ethylene-Air Flames
- Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-Wing Airplane Configuration Equipped With a Canard Control and With Wing Trailing-Edge Flap Controls
- Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04
- Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3
- Experimental techniques for predicting store motions during release or ejection
- Recent control studies
- Some Research on the Lift and Stability of Wing-Body Combinations
- An analytical evaluation of the effects of an aerodynamic modification and of stability augmenters on the pitch behavior and probable pilot opinion of two current fighter airplanes
- Effects of Components and Various Modifications on the Drag and the Static Stability and Control Characteristics of a 42 Deg Swept-Wing Fighter-Airplane Model at Mach Numbers of 1.60 to 2.50
- Boundary-Layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6
- Forty-Fourth Annual Report of the National Advisory Committee for Aeronautics Administrative Report Including Technical Reports Nos. 1342 to 1392