Hydraulic characteristics of the NACA injection impeller / by Ritter, William K.

The effect of streamlining the afterbody of an N.A.C.A. cowling / by Stickle, George W.

Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel / by Von Doenhoff, Albert E.

NACA investigation of a jet-propulsion system applicable to flight /

The propeller and cooling-air-flow characteristics of a twin-engine airplane model equipped with NACA Ds-type cowlings and with propellers of NACA 16-series airfoil sections / by McHugh, James G.

The NACA impact basin and water landing tests of a float model at various velocities and weights / by Batterson, Sidney A.

Aerodynamic and hydrodynamic tests of a family of models of flying-boat hulls derived from a streamline body NACA model 84 series / by Parkinson, John B.

Tests of a 1/17-scale model of the XBDR-1 airplane in the NACA gust tunnel / by Reisert, Thomas D.

A flight investigation of NACA aileron modifications for the improvement of the lateral control characteristics of a high-speed fighter airplane / by Williams, Walter C.

Performance tests of NACA Type A finned-tube exhaust heat exchanger / by Reuter, J. George

Wind-tunnel investigation of a spoiler-slot aileron on an NACA 23012 with a full-span Fowler flap / by Rogallo, Francis M. (Francis Melvin), 1912-2009

Tests of NACA 65(216)-420 and 66(218)-420 airfoils at high speeds / by Anderson, Joseph L.

“…NACA Wartime Reports. Series A.…”

Boundary-layer transition on the N.A.C.A. 0012 and 23012 airfoils in the 8-foot high-speed wind tunnel / by Becker, John Vernon, 1913-

Wind-tunnel investigagion of an NACA 23012 airfoil with a Handley Page slat and two flap arrangements / by Schuldenfrei, Marvin

Ditching tests with a 1/10-size model of the Army A-20A airplane. : 1 - Calm-water tests in NACA tank no. 2 / by Dawson, John R.

Flight investigaton of an NACA ice-detector suitable for use as a rate-of-icing indicator / by Gilruth, Robert R. (Robert Rowe), 1913-2000

Two-dimensional wind-tunnel investigation of two NACA low-drag airfoil sections equipped with slotted flaps and a plain NACA low-drag airfoil section for XF6U-l airplane / by Loftin, Laurence K.

Effect of compressibility on the pressures and forces acting on a modified NACA 65,3-019 airfoil having a 0.20-chord flap / by Lindsey, W. F.

Stability and control tests of a 3/4-scale model of the XP-69 airplane in the NACA full-scale tunnel / by Sweberg, Harold H.

Flight investigation of the performance and cooling characteristics of an NACA C cowling on the XP-42 airplane / by Johnston, J. Ford