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- Free-Fall Measurements of the Effects of Wing-Body Interference on the Transonic Drag Characteristics of Swept-Wing-Slender-Body Configurations
- A Free-Flight Investigation at Zero Lift in the Mach Number Range Between 0.7 and 1.4 to Determine the Effectiveness of an Inset Tab as a Means of Aerodynamically Relieving Aileron Hinge Moments
- The Influence of the Control-Surface-Servo Natural Frequency Upon the Transient Characteristics of a Flight-Path-Angle Control System Incorporating a Supersonic Missile
- Horizontal-Tail Load Measurements at Transonic Speeds of the Bell X-1 Research Airplane
- Fuselage Pressures Measured on the Bell X-1 Research Airplane in Transonic Flight
- Flight Measurements of Pressures on Base and Rear Part of Fuselage of the Bell X-1 Research Airplane at Transonic Speeds, Including Power Effects
- Flight Measurements of Lift and Drag for the Bell X-1 Research Airplane Having a 10-Percent-Thick Wing
- Formulas for the Elastic Constants of Plates With Integral Waffle-Like Stiffening
- Flow Diffusion in a Constant-Diameter Duct Downstream of an Abruptly Terminated Center Body
- An Investigation at Mach Number 2.40 of Flap-Type Controls Equipped With Overhang Nose Balances
- An Investigation at Transonic Speeds of the Effects of Fences, Drooped Nose, and Vortex Generators on the Aerodynamic Characteristics of a Wing-Fuselage Combination Having a 6-Percent-Thick, 45 Degree Sweptback Wing
- Investigation at Low Speed of the Flow Field Behind the Lifting Surfaces of a Model Equipped With a 60 Degree Triangular Wing and a 60 Degree Triangular Canard Tail
- Investigation at Mach Numbers of 1.62, 1.93, and 2.41 of the Effect of Oscillation Amplitude on the Damping in Pitch of Delta-Wing-Body Combinations
- Investigation of a Ram-Jet-Powered Helicopter Rotor on the Langley Helicopter Test Tower
- Investigation at Transonic Speeds of a Forward-Located Underslung Air Inlet on a Body of Revolution
- Wind-tunnel oscillation tests of the Bendix-Friez aerovane anemometer
- High-Resolution Autoradiography
- Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force Properties of a Full-Span, Constant-Chord, Partially Balanced Trailing-Edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26
- Wind-Tunnel Investigation to Determine the Horizontal- and Vertical-Tail Contributions to the Static Lateral Stability Characteristics of a Complete-Model Swept-Wing Configuration at High Subsonic Speeds
- Analogy Between Mass and Heat Transfer with Turbulent Flow
- The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction
- The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75
- Accelerations and passenger harness loads measured in full-scale light-airplane crashes
- Aerodynamic characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller
- An airborne indicator for measuring vertical velocity of airplanes at wheel contact
- Spiral motions of viscous fluids
- Analytical and experimental investigation of a forced-convection air-cooled internal strut-supported turbine blade
- Evaluation of a compressor bleed system for rim cooling the turbine wheel of a turbojet engine
- On the range of applicability of the transonic area rule
- Investigation of a three-blade propeller in combination with two different spinners and an NACA D-type cowl at mach numbers up to 0.80
- The flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0
- On slender-body theory at transonic speeds
- Supersonic flutter of a 60©� delta wing encountered during the flight test of a rocket-propelled model
- Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05
- Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick tapered, unswept wing
- Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord
- An investigation of the effects of a geometric twist on the aerodynamic loading characteristics of a 45©� sweptback wing-body configuration at transonic speeds
- Effects of some external-store mounting arrangements and store shapes on the buffet and drag characteristics of wingless rocket-powered models at Mach numbers from 0.7 to 1.4
- Low-pressure performance of different diameter experimental combustor liners
- Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.
- A flow calorimeter for determining combustion efficiency from residual enthalpy of exhaust gases
- Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds
- Effects of fences, leading-edge chord-extensions, bound-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60©� sweptback-wing--indented-body configuration at transonic speeds
- The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds
- An experimental transonic investigation of a 45©� sweptback wing-body combination with several types of body indentation with theoretical comparisons included
- Effects of Wing Leading-Edge Camber and Tip Modifications on the Aerodynamic Characteristics of a 1/20-Scale Model of the Convair F-102 Airplane at Transonic Speeds
- Measurement of the Static Stability and Control and the Damping Derivatives of a 0.13-Scale Model of the Convair XFY-1 Airplane, TED No. NACA DE 368
- Flight Results from a 1/10-Scale Rocket Model of the Lockheed XF-104 Airplane at Transonic Mach Numbers
- Longitudinal Control Characteristics of a 1/20-Scale Model of the Convair F-102 Airplane at Transonic Speeds
- Preliminary Data on the Effects of Inlet Pressure Distortions on the J57-P-1 Turbojet Engine