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Decade: 1930-1939

Serial/Series Title: NACA Technical Notes

Collection: Technical Report Archive and Image Library

Results 1 - 24 of 411

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The 6-foot-4-inch wind tunnel at the Washington Navy Yard

The 6-foot-4-inch wind tunnel at the Washington Navy Yard

An accurate method of measuring the moments of inertia of airplanes

An accurate method of measuring the moments of inertia of airplanes

Adhesion of ice in its relation to the de-icing of airplanes

Adhesion of ice in its relation to the de-icing of airplanes

Advantages of oxide films as bases for aluminum pigmented surface coatings for aluminum alloys

Advantages of oxide films as bases for aluminum pigmented surface coatings for aluminum alloys

The aerodynamic analysis of the gyroplane rotating-wing system

The aerodynamic analysis of the gyroplane rotating-wing system

The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear

The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear

The aerodynamic characteristics of airfoils as affected by surface roughness

The aerodynamic characteristics of airfoils as affected by surface roughness

The aerodynamic characteristics of airfoils at negative angles of attack

The aerodynamic characteristics of airfoils at negative angles of attack

Aerodynamic characteristics of anemometer cups

Aerodynamic characteristics of anemometer cups

Aerodynamic characteristics of several airfoils of low aspect ratio

Aerodynamic characteristics of several airfoils of low aspect ratio

The aerodynamic characteristics of six commonly used Airfoils over a large range of positive and negative angles of attack

The aerodynamic characteristics of six commonly used Airfoils over a large range of positive and negative angles of attack

The aerodynamic characteristics of three tapered airfoils tested in the variable density wind tunnel

The aerodynamic characteristics of three tapered airfoils tested in the variable density wind tunnel

The aerodynamic drag of five models of side floats N.A.C.A. Models 51-E, 51-F, 51-G, 51-H, 51-J

The aerodynamic drag of five models of side floats N.A.C.A. Models 51-E, 51-F, 51-G, 51-H, 51-J

The aerodynamic drag of flying-boat hull model as measured in the NACA 20-foot wind tunnel I.

The aerodynamic drag of flying-boat hull model as measured in the NACA 20-foot wind tunnel I.

The aerodynamic effect of a retractable landing gear

The aerodynamic effect of a retractable landing gear

Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model

Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model

The aerodynamic forces and moments on a spinning model of the F4B-2 airplane as measured by the spinning balance

The aerodynamic forces and moments on a spinning model of the F4B-2 airplane as measured by the spinning balance

Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by spinning balance

Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by spinning balance

Aerodynamic tests of a low aspect ratio tapered wing with an auxiliary airfoil for use on tailless airplanes

Aerodynamic tests of a low aspect ratio tapered wing with an auxiliary airfoil for use on tailless airplanes

Aerodynamic tests of a low aspect ratio tapered wing with various flaps, for use on tailless airplanes

Aerodynamic tests of a low aspect ratio tapered wing with various flaps, for use on tailless airplanes

Alterations and tests of the "Farnboro" engine indicator

Alterations and tests of the "Farnboro" engine indicator

Analysis and model tests of autogiro jump take-off

Analysis and model tests of autogiro jump take-off

Analysis of a strut with a single elastic support in the span, with applications to the design of airplane jury-strut systems

Analysis of a strut with a single elastic support in the span, with applications to the design of airplane jury-strut systems

Analytical determination of the load on a trailing edge flap

Analytical determination of the load on a trailing edge flap

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