Browse TRAIL Inventories

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degrees Sweepback: Estimated Downwash Angles Derived From Pressure Measurements on the Tail at Mach Numbers of 1.40 and 1.59

Tables for the computation of wave drag of arrow wings of arbitrary airfoil section

Tables for the Computation of Wave Drag of Arrow Wings of Arbitrary Airfoil Section

The proper combination of lift loadings for least drag on a supersonic wing

Span loadings due to wing twist at transonic and supersonic speeds

The use of pure twist for drag reduction on arrow wings with subsonic leading edges

A tabulation of wind-tunnel pressure data at Mach numbers of 1.61 and 2.01 of five swept wings of the same plan form but different surface shapes


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