Low-speed investigation of a small triangular wing of aspect ratio 2.0 III : static stability with twin vertical fins
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Rose, Leonard↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel II : the Effectiveness and Hinge Moments of a Constant-chord Plain Flap
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Stephenson, Jack D↗
High-speed wind-tunnel investigation of a sweptback wing with an added triangular area at the center
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Henry, Beverly, Z , jr↗
Aerodynamic Characteristics at Subsonic and Supersonic Mach Numbers of a Thin Triangular Wing of Aspect Ratio 2 I : Maximum Thickness at 20 Percent of the Chord
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Berggren, Robert E↗
Preliminary Wind-Tunnel Tests of Triangular and Rectangular Wings in Steady Roll at Mach Numbers of 1.62 and 1.92
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Brown, Clinton E↗
Full-scale Investigation of the Maximum Lift and Flow Characteristics of an Airplane Having Approximately Triangular Plan Form
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Wilson, Herbert A , Jr↗
An Investigation at Low Speed of a Large-scale Triangular Wing of Aspect Ratio Two II : the Effect of Airfoil Section Modifications and the Determination of the Wake Downwash
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Anderson, Adrien E↗
Investigation of Wing Characteristics at a Mach Number of 1.53 I : Triangular Wings of Aspect Ratio 2
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Vincenti, Walter G↗
Low-speed Investigation of a Small Triangular Wing of Aspect Ratio 2.0 I : the Effect of Combination with a Body Revolution and Height Above a Ground Plane
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Rose, Leonard M↗
Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel I : the Effect of Reynolds Number and Mach Number on the Aerodynamic Characteristics of the Wing with Flap Undeflected
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Edwards, George G↗
Preliminary Tests at Supersonic Speeds of Triangular and Swept-back Wings
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Ellis, Macon C , Jr↗
Wing-flow Tests of a Triangular Wing of Aspect Ratio Two I : Effectiveness of Several Types of Trailing-edge Flaps on Flat-plate Models
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FLAPS - COMPLETE WINGS↗
Wind-tunnel Investigation at a Mach Number of 1.53 of an Airplane with a Triangular Wing
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Scherrer, Richard↗
A theoretical investigation of the dynamic lateral oscillatory stability of an airplane having a 60 degree triangular wing
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Johnson, Joseph L↗
Low-speed Investigation of a Small Triangular Wing of Aspect Ratio 2.0 II : Flaps on Flat-plate Models
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Rose, Leonard M↗
Investigation of Downwash and Wake Characteristics at a Mach Number of 1.53 II : Triangular Wing
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Perkins, Edward W↗
Wind-tunnel Investigation of a Tailless Triangular-wing Fighter Aircraft at Mach Numbers from 0.5 to 1.5
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Lawrence, Leslie F↗
Chordwise and Spanwise Loadings Measured at Low Speed on Large Triangular Wings
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Anderson, Adrien E↗