A Preliminary Investigation at Mach Number 1.91 of a Diffuser Employing a Pivoted Cone to Improve Operation at Angle of Attack
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Beheim, Milton A↗
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Results for “Angle of attack”
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Rocket-powered Model Investigation of Lift, Drag, and Stability of a Body-tail Configuration at Mach Numbers from 0.8 to 2.3 and Angles of Attack Between plus or Minus 6.5 Degrees
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Gillespie, Warren, Jr↗
Angle-of-attack-supersonic performance of a configuration consisting of a ramp-type scoop inlet located either on top or bottom of a body of revolution
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Kremzier, Emil J↗
Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 1.45 and 1.97
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings of aspect ratios 2 and 4 at Mach numbers of 1.45 and 1.97. The investigation includes some comparison of the effects of Reynolds number and of thickening the wing root sections on the loading.
Kaattari, George E↗
Effect of Rotation of a NACA 1-series E-type Cowling on the Internal Flow and Force Characteristics of the Cowling at Mach Numbers up to 0.84 and at an Angle of Attack of 0 Degrees
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Sammonds, Robert I↗
Wind-tunnel investigation of effect of sweep on rolling derivatives at angles of attack up to 13 degrees and at high subsonic Mach numbers, including a semiempirical method of estimating the rolling derivatives
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Wiggins, James W↗
Low-speed Measurement of Static Stability and Damping Derivatives of a 60 Degree Delta-wing Model for Angles of Attack of 0 Degrees to 90 Degrees
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Hewes, Donald E↗
Effect of Fuselage Fences on the Angle-of-attack Supersonic Performance of a Top-inlet - Fuselage Configuration
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Kremzier, Emil J↗
Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 2.46 and 3.36
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings of aspect ratios 2 and 4 at Mach numbers of 2.46 and 3.36. The investigation includes some comparison of the effects of Mach number, Reynolds number, and thickening the wing root sections on the loading.
Kaattari, George E↗
A Flight Investigation at Transonic Speeds and Small Angles of Attack of the Aerodynamic Characteristics of a Model Having a 45 Degree Sweptback Wing of Aspect Ratio 3 with an Naca 64A006 Airfoil Section
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Holdaway, George H↗
Effects of Angle of Attack and Airfoil Profile on the Two-dimensional Flutter Derivatives for Airfoils Oscillating in Pitch at High Subsonic Speeds
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Wyss, John A↗
Investigation of a Ramp-type Inlet Designed for Improved Angle-of-attack Performance at Mach Number 2.0
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Wise, G A↗
Effect of automatic stabilization on the sideslip and angle-of-attack disturbances in rolling maneuvers
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Gates, Ordway B , Jr↗
Load distributions on wings and wing-body combinations at high angles of attack and supersonic speeds
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Katzen, Elliott D↗
Theoretical investigation of the effects of configuration changes on the center of pressure shift of a body-wing-tail combination due to angle of attack and Mach number at transonic and supersonic speeds
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Spahr, J Richard↗
Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region
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Pierce, Harold B↗
An Experimental Investigation of the Flow Phenomena over Bodies at High Angles of Attack at a Mach Number of 2.01
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Gapcynski, John P↗
Comparison Between Analytical and Wind-tunnel Results on Flutter of Several Low-aspect-ratio, High-density, Unswept Wings at High Subsonic Speeds and Zero Angle of Attack
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WARNER ROBERT W↗