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The Comper "Streak" Single Seat Airplane (British): A Low-Wing Cantilever...

Circular describing the Comper Streak single-seat low-wing cantilever monoplane. Details of the fuselage, construction, wing, stabilizer, engine, landing gear, characteristics, drawings, and...

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Flight Measurements of the Effect of Various Amounts of Aileron Droop on the...

Report presenting tests of the low-speed lateral-control characteristics of an observation airplane with ailerons and spoilers in combination and with the spoilers disconnected and the ailerons used...

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The Lagrangian Multiplier Method of Finding Upper and Lower Limits to...

"The theory of Lagrangian multipliers is applied to the problem of finding both upper and lower limits to the true compressive buckling stress of a clamped rectangular plate. The upper and lower limits...

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An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane...

Report presenting an investigation of a thermal ice-prevention system for a Curtiss-Wright C-46 airplane, including the equipment for the wings, empennage, and windshield. The report is the third in a...

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Lioré-Olivier Airplane: Type 12 Night-Bomber or Type 20 Commercial

Report presenting a description of the Lioré-Olivier Type 12 night bomber, which can also be converted into the Type 20 commercial. A description of the cell of the wings, fuselage, power plant,...

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A Concise Theoretical Method for Profile-Drag Calculation; Advance Report

In this report a method is presented for the calculation of the profile drag of airfoil sections. The method requlres only a knowledge of the theoretical velocity distribution and can be applied...

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D.H. 86 "Express Air Liner" (British): A Four-Engine Biplane

Circular describing the De Havilland Express Air Liner, which is a four-engine two-bay biplane of clean and well-streamlined form. Details of the cabin, controls, fuselage, tail, wings, engines,...

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On the Flow of a Compressible Fluid by the Hodography Method 1: Unification...

Report presenting elementary basic solutions of the equations of motion of a compressible fluid in the hodograph variables are developed and used to provide a basis for comparison in the form of...

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Blériot-Spad 91 Airplane (French): Pursuit Single-Seater, Type "Jockey"

Report presenting a description of the design of the Blériot-Spad 91 airplane. This aircraft has announced a speed of 270 km per hour at 4000 m. It is of all metal construction.

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Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force...

Report presenting a free-flight investigation of a rocket-powered research model to determine the hinge-moment and normal-force characteristics of a trailing-edge control on a delta wing between Mach...

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An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane...

Report presenting flight tests conducted to evaluate the effect of a thermal ice prevention system on the aerodynamic performance of a C-46 cargo airplane. The installation of the thermal...

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Effect of Roughness on Properties of Airfoils

The first group of a large series of contemplated experiments on the effect of roughness was intended to show the effect of great roughness on airfoils of various sizes and attitudes.

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Les Mureaux "130.a2" Observation Airplane (French): A High-Wing Two-Seat...

Circular presenting Les Mureaux 130.A2, which is a high-wing two-seat observation monoplane. A description of the design, performances, components, performance qualities, photographs, and drawings are...

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Reciprocity relations in aerodynamics

From Introduction: "The purpose of the present paper is twofold. First, a close connection will be established between reverse-flow theorems in subsonic and supersonic, steady-state wing theory and...

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The Bernard 80 G.R. Long-Distance Airplane (French) : A Two-Place Cantilever...

Circular presenting a description of the Bernard 80 aircraft. Details are provided on the body shape, wings, ribs, fuel requirements, and flight characteristics.

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The S.P.C.A. 30 M.4 Military Airplane (French): A Multiplace Low-Wing Airplane

Circular describing the S.P.C.A. 30 M.4 multiplace, which is an aircraft designed to carry four people that can be used as a fighter aircraft or a day or night bomber. Details of the design,...

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Wind-Tunnel Investigation of the Effects of Spoilers on the Characteristics...

Report discussing the effects of circular-arc spoilers on the section characteristics of an NACA 66,2-216 airfoil with a 0.25-chord slotted flap. Spoilers were tested on the upper surface of the...

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The S.A.B.C.A. "S.XI" Commercial Airplane (Belgian): A High-Wing...

Circular describing the S.A.B.C.A. S.XI commercial airplane, which is a high-wing semicantilever monoplane. Details of the history of its creation, its design, components, engines, fuel tanks,...

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Lift Theory of Supporting Surfaces: Second Article

Memorandum presenting a description of the hydrodynamic lift theory of supporting services. This report is mainly about the task of finding suitable wing sections for given lift conditions. Formulas...

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An Experimental Investigation of Rectangular Exhaust-Gas Ejectors Applicable...

Report presenting an experimental investigation of rectangular exhaust-gas ejector pump to provide data that would serve as a guide to the design of ejector applications for aircraft engines with...

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