Leading-edge deflection optimization for a highly swept arrow-wing configuration / by Coe, Paul L., Huffman, Jarrett K., Fenbert, James W.

Online Access
Online Access

Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow / by Watkins, Charles E.

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

Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips. : Subsonic leading edges / by Margolis, Kenneth

An investigation of aircraft heaters. : 38 - Determination of thermal performance of rectangular- and trapezoidal-shaped inner-skin passages for anti-icing systems / by Boelter, L. M. K. (Llewellyn Michael Kraus), 1898-1966

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.

Effects of boundary-layer displacement and leading-edge bluntness on pressure distribution, skin friction, and heat transfer of bodies at hypersonic speeds / by Bertram, Mitchel H.

Estimation of the damping in roll of supersonic-leading-edge wing-body combinations / by Tucker, Warren A.

The dynamic lateral control characteristics of airplane models having unswept wings with round- and sharp-leading-edge sections / by Hassell, James L.

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.

Effects of modifications to the leading-edge region on the stalling characteristics of the NACA 63₁-012 airfoil section / by Kelly, John A.

Lift and pitching derivatives of thin sweptback tapered wings with streamwise tips and subsonic leading edges at supersonic speeds / by Malvestuto, Frank S.

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.

A factor affecting transonic leading-edge flow separation / by Wood, George P.

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

Some observations on maximum pressure rise across shocks without boundary-layer separation on airfoils at transonic speeds / by Lindsey, W. F.

On slender delta wings with leading-edge separation / by Brown, Clinton E.

Effect of leading-edge geometry on boundary-layer transition at Mach 3.1 / by Brinich, Paul F.

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

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.