Wind tunnel investigation of control surface characteristics. : 12 - Various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal... by Hoggard, H. Page

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Effect in flight of the propeller cuffs and spinner on pressure recovery in front of a double-row radial aircraft engine in a twin-engine airplane / by Ellisman, Carl

The effect of Mach number on the aerodynamic characteristics of a single-engine pursuit airplane as determined from tests of a 1/3-scale model / by Robinson, Robert C.

“…NACA Wartime Reports. Series A.…”

A comparison of the effects of four-blade dual- and single-rotation propellers on the stability and control characteristics of a high-powered single-engine airplane / by Harper, Charles W.

“…NACA Wartime Reports. Series A.…”

WInd-tunnel investigation of effects of a pusher propeller on lift, profile drag, pressure distribution, and boundary-layer transition of a flapped wing / by Sandahl, Carl A.

The effect of stability and control of a pusher propeller behind conventional tail surfaces as determined by tests of a powered model in the free-flight tunnel / by Campbell, John P.

Tests of a 0.1475c aileron with a tab on low-drag section for Curtiss XP-60 airplane in the low-turbulence tunnel / by Von Doenhoff, Albert E.

Wind-tunnel investigation of plain ailerons for a wing with a full-span flap consisting of an inboard Fowler and an outboard retractable split flap / by Harris, Thomas A.

Wind-tunnel investigation of a full-span retractable flap in combination with full-span plain and internally balanced ailerons on a tapered wing / by Rogallo, Francis M. (Francis Melvin), 1912-2009

Cylinder-head cooling by means of a shield in the exhaust passage / by Wilsted, H. D.

A method of estimating the knock rating of hydrocarbon fuel blends / by Sanders, Newell D.

A preliminary investigation of exhaust-gas ejectors for ground cooling / by Manganiello, Eugene J.

Stability of a body stabilized by fins and suspended from an airplane / by Phillips, W. H.

A description of the Ju 88 airplane anti-icing equipment / by Rodert, Lewis A.

“…NACA Wartime Reports. Series A.…”

Compressible potential flow with circulation about a circular cylinder / by Heaslet, M. A. (Maxwell Alfred), 1907-

“…NACA Wartime Reports. Series A.…”

Wind-tunnel investigation of ailerons on a low-drag airfoil. : 3 - The effect of tabs / by Holtzclaw, Ralph W.

“…NACA Wartime Reports. Series A.…”

Considerations of wake-excited vibratory stress in a pusher propeller / by Corson, Blake W.

Theoretical distribution of load over a swept-back wing / by Cohen, Doris

Pressure distribution over an airfoil with a balanced split flap / by Ames, Milton B.

Effects of a simulated ice formation on the aerodynamic characteristics of an airfoil / by Gulick, Beverly G.