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- Investigation of Spoilers at a Mach Number of 1.93 to Determine the Effects of Height and Chordwise Location on the Section Aerodynamic Characteristics of a Two-Dimensional Wing
- Investigation of Tantalum in a 3,800 Degrees Fahrenheit Supersonic Airstream
- Investigation of Flutter Characteristics of Three Low-Aspect-Ratio All-Movable Half-Span Control Surfaces at Mach Numbers From 1.49 to 2.87
- Investigation of the Longitudinal Aerodynamic Characteristics of a Trapezoidal-Wing Airplane Model With Various Vertical Positions of Wing and Horizontal Tail at Mach Numbers of 1.41 and 2.01
- Analysis of Turbulent Flow and Heat Transfer in Noncircular Passages
- Experimental Investigation of the Lateral Trim of a Wing-Propeller Combination at Angles of Attack Up to 90 Degrees With All Propellers Turning in the Same Direction
- Theoretical Calculations of Supersonic Wave Drag at Zero Lift for a Particular Store Arrangement
- Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-Oxygen Mixtures Assuming Equilibrium Composition
- Theoretical Rocket Performance of Liquid Methane with Several Fluorine-Oxygen Mixtures Assuming Frozen Composition
- Hydrodynamic Characteristics of a Model of a Proposed Six-Engine Hull-Type Seaplane Designed for Supersonic Flight
- Flight Tests of Two Smoke-Producing Devices Having Deacon Rocket Boosters
- Heat Transfer for Mach Numbers Up to 2.2 and Pressure Distributions for Mach Numbers Up to 4.7 From Flight Investigations of a Flat-Face-Cone and a Hemisphere-Cone
- Heat Transfer Measured on a Flat-Face Cylinder-Flare Configuration in Free Flight at Mach Numbers From 1.6 to 2.7
- Further Investigation of Fatigue-Crack Propagation in Aluminum-Alloy Box Beams
- Heat-Transfer and Pressure Measurements From a Flight Test of the Second 1/18-Scale Model on the Titan Intercontinental Ballistic Missile Up to a Mach Number of 3.91 and Reynolds Number Per Foot of 23.4 X 10(Exp 6) : Coord. No. AF-AM-70
- 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
- Spin-Tunnel Investigation of a 1/28-Scale Model of a Subsonic Attack Airplane
- Spin Tunnel Investigation of a 1/30 Scale Model of the North American A-5A Airplane
- Flow and Drag Formulas for Simple Quadrics
- Graphic Construction of Joukowski Wings
- The Aerodynamic Forces on Airship Hulls
- Applications of Modern Hydrodynamics to Aeronautics Part 1: Fundamental Concepts and the Most Important Theorems. Part 2: Applications
- The Minimum Induced Drag of Aerofoils
- Flow and Force Equations for a Body Revolving in a Fluid
- Determination of the local heat-transfer characteristics on glaze ice accretions on a cylinder and a NACA 0012 airfoil
- The Theory of the Pitot and Venturi Tubes, Part 2
- Unsteady flow past a NACA 0012 airfoil pitching at constant rates