Investigation of the boundary layer about a symmetrical airfoil in a wind tunnel of low turbulence / by Von Doenhoff, Albert E.

Some lift and drag measurements of a representative bomber nacelle on a low-drag wing. : Part 1 / by Ellis, Macon C.

Some lift and drag measurements of a representative bomber nacelle on a low-drag wing. : Part 2 / by Ellis, Macon C.

Wind-tunnel investigation of a low-drag airfoil section with a double slotted flap / by Bogdonoff, Seymour M.

A metallurgical investigation of a large forged disc of low-carbon N-155 alloy / by Freeman, J. W. (James W.)

WInd-tunnel tests of ailerons at various speeds. : 4 - Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt-nose balance on the NACA 23012 airfoil... by Letko, W.

A preignition indicator for aircraft engines / by Dallas, Thomas

Performance charts for a turbojet system / by Pinkel, Benjamin, 1909-

A method for studying piston friction / by Forbes, J. E.

A study of piston and ring friction / by Leary, W. A.

Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour / by Bird, J. D.

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Tests of a thermal ice-prevention system for a wing leading-edge landing-light installation / by Hillendahl, Wesley H.

“…NACA Wartime Reports. Series A.…”

A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane / by Johnson, Harold I.

Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane / by Kayten, Gerald G.

The locus of possible positions of a heavy bomber in space after a 12-second time interval / by Mathews, Charles W.

Wind-tunnel investigation of a plain aileron with various trailing-edge modifications on a tapered wing. : 3 - Ailerons with simple and spring-linked balancing tabs / by Rogallo, Francis M. (Francis Melvin), 1912-2009

Wind-tunnel investigation of control-surface characteristics. : 22 - Medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.20-airfoil-chord fl... by Riebe, John M.

Effect of blade loading on the climb and high-speed performance of a three-blade Hamilton standard no. 6507A-2 propeller on a Republic P-47D airplane / by Gardner, John J.

Preliminary tank tests of an outboard float having the form of a streamline body of revolution fitted with a hydrofoil / by King, Douglas A.

The effects of angle of dead rise and angle of afterbody keel on the resistance of a model of a flying-boat hull / by Bell, Joe W.