Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds : Subsonic leading edges and trailing edges / by Malvestuto, Frank S.

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Formulas and charts for the supersonic lift and drag of flat swept-back wings with interacting leading and trailing edges / by Cohen, Doris

Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds. : Supersonic leading and trailing edges / by Harmon, Sidney M.

Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the Mach line... by Goin, Kennith L.

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Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities / by Chapman, Dean R.

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Estimation of low-speed lift and hinge-moment parameters for full-span trailing-edge flaps on lifting surfaces with and without sweepback / by Dods, Jules B.

On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream / by Ribner, H. S. (Herbert S.), 1913-

Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper. : Mach lines behnid flap leading and trailing edges / by Kainer, Julian H.

Supersonic lift and pitching moment of thin sweptback tapered wings produced by constant vertical acceleration. : Subsonic leading edges and supersonic trailing edges / by Malvestuto, Frank S.

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Exploratory investigation of an airfoil with area suction applied to a porous, round trailing edge fitted with a lift-control vane / by Dannenberg, Robert E.

Reduction of profile drag at supersonic velocities by the use of airfoil sections having a blunt trailing edge / by Chapman, Dean R.

Experimental investigation of the forces and moments due to sideslip of a series of triangular vertical- and horizontal-tail combinations at Mach numbers of 1.62, 1.93, and 2.41 / by Coletti, Donald E.

Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics / by Stewart, Warner L.

Effect of trailing-edge thickness on lift at supersonic velocities / by Chapman, Dean R.

Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lif... by Morrow, John D.

Measurements of the effect of trailing-edge thickness on the zero-lift drag of thin low-aspect-ratio wings / by Morrow, John D.

Comparison of theoretical stresses and deflections of multicell wings with experimental results obtained from plastic models / by Zender, George W.

Theoretical investigation of velocity diagrams of a single-stage turbine for a turbojet engine at maximum thrust per square foot turbine frontal area / by Cohen, Leo

Effect of a finite trailing-edge thickness on the drag of rectangular and delta wings at supersonic speeds / by Klunker, E. B.

Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings w... by Hannah, Margery E.