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- Some notes on the aerodynamic loads associated with external-store installations
- Factors affecting transition at supersonic speeds
- Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading
- Fuel characteristics pertinent to the design of aircraft fuel systems.Supplement 1 - Additional information on MIL-F-7914(AER) Grade JP-5 fuel and several fuel oils
- Average skin-friction drag coefficients from tank tests of a parabolic body of revolution (NACA RM-10)
- Effect of longitudinal wings position on the pressure characteristics at transonic speeds of a 45©� sweptback wing-fuselage model
- Recent Results Pertaining to the Application of the "Area Rule"
- Rocket-Model Investigation of the Longitudinal Stability, Drag, and Duct Performance Characteristics of the North American MX-770 (X-10) Missile at Mach Numbers from 0.80 to 1.70
- Notes on the Prediction of Shock-induced Boundary-layer Separation
- Flow Coefficients for Orifices in Base of Transpiration-Cooled Turbine Rotor Blade
- Preliminary Transient Performance Data on the J73 Turbojet Engine, 3, Altitude, 45,000 Feet
- Preliminary Transient Performance Data on the J73 Turbojet Engine. II - Altitude, 35,000 Feet
- Theory of Wing-Body Drag at Supersonic Speeds
- Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration have a 60©� delta wing and a high unwept horizontal tail
- Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6©� and NACA 65A006 airfoil section
- Control hinge-movement and effectiveness characteristics of several interchangeable tip controls on a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96
- Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of the 45©� sweptback-wing--body combination
- An experimental and theoretical investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic characteristics in sideslip of an unswept, untapered tail assembly
- Impingement of Droplets in 90 deg Elbows with Potential Flow
- Impingement of Water Droplets on NACA 65A004 Airfoil and Effect of Change in Airfoil Thickness from 12 to 4 Percent at 4 deg Angle of Attack
- A Method for Determining Cloud-Droplet Impingement on Swept Wings
- Comparison of Several Methods of Cyclic De-Icing of a Gas-Heated Airfoil
- Component and over-all performance evaluation of a J47-GE-25 turbojet engine over a range of engine-inlet Reynolds number indices
- Some effects of aeroelasticity and sweepback on the rolling effectiveness and drag of a 1/11-scale model of the Bell X-5 airplane wing at Mach numbers from 0.6 to 1.5
- Investigation of gases evolved during firing of vitreous coatings on steel
- A fundamental investigation of fretting corrosion
- High-frequency pressure indicators for aerodynamic problems
- Investigation of lateral control near the stall flight investigation with a light high-wing monoplane tested with various amounts of washout and various lengths of leading-edge slot
- Interim report on a fatigue investigation of a full-scale transport aircraft wing structure
- Investigation of sandwich construction under lateral and axial loads
- A method for stabilizing shock waves in channel flow by means of a surge chamber
- A method of deriving frequency-response data for motion of the center of gravity from data measured on an aircraft at locations other than the center of gravity
- The flow about a section of a finite-aspect-ratio NACA 0018 airfoil on a transonic bump
- Optimum controllers for linear closed-loop systems
- On the use of a damped sine-wave elevator motion for computing the design maneuvering horizontal-tail load
- On traveling waves in beams
- One-dimensional, compressible, viscous flow relations applicable to flow in a ducted helicopter blade
- New experiments on impact-pressure interpretation in supersonic and subsonic rarefied air streams
- A new shadowgraph technique for the observation of conical flow phenomena in supersonic flow and preliminary results obtained for a triangular wing
- Matrix methods for determining the longitudinal-stability derivatives of an airplane from transient flight data
- Preliminary experimental investigation of low-speed turbulent boundary layers in adverse pressure gradients
- Propeller-noise charts for transport airplanes
- Lift and pitching moment at low speeds of the naca 64A010 airfoil section equipped with various combinations of a leading-edge slat, leading-edge flap, split flap, and double-slotted flap
- Low-speed drag of cylinders of various shapes
- Heat and momentum transfer between a spherical particle and air streams
- Icing protection for a turbojet transport airplane : heating requirements methods of protection, and performance penalties
- Impingement of water droplets on a cylinder in an incompressible flow field and evaluation of rotating multicylinder method for measurement of droplet-size distribution, volume-median droplet size, and liquid-water content in clouds
- Friction and wear investigation of molybdenum disulfide I : effect of moisture
- Heat transfer and skin friction by an integral method in the compressible laminar boundary layer with a streamwise pressure gradient
- Water-landing investigation of a flat-bottom v-step model and comparison with a theory incorporating planing data