The Effect of Aspect Ratio on the Subsonic Aerodynamic Characteristics of Wings with NACA 65(sub 1)-210 Sections
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Nelson, Warren, H↗
Engineering topics
Erickson, Albert L
Publications and source records attributed to Erickson, Albert L.
Wind-tunnel Investigation of Transonic Aileron Flutter
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Erickson, Albert L↗
Some Preliminary Results in the Determination of Aerodynamic Derivatives of Control Surfaces in the Transonic Speed Range by Means of a Flush-type Electrical Pressure Cell
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Erickson, Albert L↗
Wind-tunnel Investigation of Transonic Aileron Flutter of a Semispan Wing Model with an NACA 23013 Section
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Perone, Angelo↗
A Suggested Method of Analyzing for Transonic Flutter of Control Surfaces Based on Available Experimental Evidence
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Erickson, Albert L↗
Wind-Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes
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AIRPLANES- LOCKHEED P-38 WIND TUNNEL TESTS - (AAL-↗
Investigation of Diving Moments of a Pursuit Airplane in the Ames 16-Foot High Speed Wind Tunnel
A pursuit type airplane encountered severe diving moments in high-speed dives which make recovery difficult. For the purpose of investigating these diving moments and finding means for their reduction, a 1/6-scale model of the airplane was tested in the 16-foot high-speed wind tunnel at Ames Aeronautical Laboratory. The test results indicate that up to a Mach number of at least 0.75, the limit of the tests, the dive-recovery difficulties can be alleviated and the longitudinal maneuverability improved by the substitution of a long symmetrical fuselage for the standard fuselage.
MACH NUMBER↗