A preliminary investigation of the usefulness of camber in obtaining favorable airfoil-section drag characteristics at supercritical speeds
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Nitzberg, Gerald E↗
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Results for “Camber”
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Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effects at Subsonic Speeds of a Constant-chord Elevon on a Wing Cambered and Twisted for a Uniform Load at a Lift Coefficient of 0.25
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Jones, J Lloyd↗
Preliminary Aerodynamic Investigation of the Effect of Camber on a 60 Degree Delta Wing with Round and Beveled Leading Edges
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Riebe, John M↗
Performance of High-pressure-ratio Axial-flow Compressor Using Highly Cambered NACA 65-series Blower Blades at High Mach Numbers
A complete stage of an axial-flow compressor was designed and built to investigate the possibility of obtaining a high pressure ratio with an acceptable efficiency through the use of the optimum combination of high blade loading and high relative inlet Mach number. Over-all stage performance was investigated over a range of flows at equivalent tip speeds of 418 to 836 feet per second. At design speed (836 ft/sec), a peak total-pressure ration of 1.445 was obtained with an adiabatic efficiency of 0.89. For design angle of attack at the mean radius, a total-pressure ratio of 1.392 was obtained.
COMPRESSORS - AXIAL FLOW↗
Effects of twist and camber on the low-speed characteristics of a large-scale 45 degree swept-back wing
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Hunton, Lynn W↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Characteristics at Supersonic Speeds of a Model with the Wing Twisted and Cambered for Uniform Load
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Hall, Charles F↗
Effect of Compressibility and Camber as Determined from an Investigation of the NACA 4-(3)(08)-03 and 4-(5)(08)-03 Two-blade Propellers up to Forward Mach Numbers of 0.925
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Carmel, Melvin M↗
Wind-tunnel Investigation at Low Speed of a Wing Swept-back 63 Degrees and Twisted and Cambered for a Uniform Load at a Lift Coefficient of 0.5
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Weiberg, James A↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effect of Sideslip on Aerodynamic Characteristics at a Mach Number of 1.4 with the Wing Twisted and Cambered
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Lessing, Henry C↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effectiveness of an Elevon as a Longitudinal Control and the Effects of Camber and Twist on the Maximum Lift-drag Ratio at Supersonic Speeds
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Olson, Robert N↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effect of Reynolds Number at Supersonic Mach Numbers on the Longitudinal Characteristics of a Wing Twisted and Cambered for Uniform Load
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Heitmeyer, John C↗
Wind-tunnel Investigation at Low Speed of a Wing Swept Back 63 Degrees and Twisted and Cambered for Uniform Load at a Lift Coefficient of 0.5 and with a Thickened Tip Section
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Weiberg, James A↗
The Effects of Increasing the Leading-edge Radius and Adding Forward Camber on the Aerodynamic Characteristics of a Wing with 35 Degrees of Sweepback
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Demele, Fred A↗
The effect of blade-section camber on the static characteristics of three NACA propellers
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Wood, John H↗
The Effects of Mach Number and Reynolds Number on the Aerodynamic Characteristics of Several 12-percent-thick Wings Having 35 Degrees of Sweepback and Various Amounts of Camber
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Tinling, Bruce E↗
Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 4 with NACA 0005-63 thickness distribution, cambered and twisted for trapezoidal span load distribution
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Phelps, E Ray↗
Low-speed Characteristics of a Wing Having 63 Degrees Sweepback and Uniform Camber
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Rose, Leonard M↗
The Effects of Camber and Twist on the Aerodynamic Loading and Stalling Characteristics of a Large-scale 45 Degree Swept-back Wing
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Hunton, Lynn W↗