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- 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
- Free-Flight Tests of 0.11-Scale North American F-100 Airplane Wings to Investigate the Possibility of Flutter in Transonic Speed Range at Varying Angles of Attack
- Free-Flight Tests of 1/9-Scale Convair YF-102 Airplane Wings at Transonic and Supersonic Speeds to Investigate the Possibility of Flutter
- Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45©� sweptback wing at transonic speeds
- The twisting effect at transonic speeds of spoiler ailerons on a 45©� sweptback, aspect-ratio-4, tapered wing
- Wind-tunnel investigation at high subsonic speeds to determine the rolling derivatives of two wing-fuselage combinations having triangular winds, including a semiempirical method of estimating the rolling derivatives
- Free-flight measurements of the rolling effectiveness and drag of trailing-edge spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.4
- Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45©� sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶
- Theoretical investigation of some discontinuous yaw dampers
- Flight investigation of an aileron and a spoiler on a wing of the X-3 airplane plan form at Mach numbers from 0.5 to 1.6
- Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds
- Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail
- Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine
- A Method for Prevention of Screaming in Rocket Engines
- Variation of Local Liquid-Water Concentration About and Ellipsoid of Fineness Ratio 5 Moving in a Droplet Field
- Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section