Resource Type

Armstrong-Whitworth A.W. 15 "Atlanta" Airplane (British): A Commercial Multiplace Cantilever Monoplane (open access)

Armstrong-Whitworth A.W. 15 "Atlanta" Airplane (British): A Commercial Multiplace Cantilever Monoplane

Circular describing the Armstrong Whitworth XV "Atalanta" airplane, which is a commercial multiplace cantilever monoplane. Details of the wings, landing gear, fuselage, control surfaces, structural design, wing, engine, characteristics, drawings, and photographs are provided.
Date: August 1932
Creator: unknown
System: The UNT Digital Library
The Bleriot 137 Military Airplane (French): A Twin-Engine Multiplace Monoplane (open access)

The Bleriot 137 Military Airplane (French): A Twin-Engine Multiplace Monoplane

Circular presenting a description of the Blériot 137, which is a metal modification of the Bléirot 127. A description of the crew, the equipment, firing tests of the guns, and flight characteristics are provided.
Date: August 1932
Creator: unknown
System: The UNT Digital Library
The Latécoère 501 Commercial Seaplane (French): A Three-Engine Metal Sesquiplane (open access)

The Latécoère 501 Commercial Seaplane (French): A Three-Engine Metal Sesquiplane

Circular presenting a description of the Latécoère 501. A more detailed description of the general characteristics, power plant, wings, planing fins, hull, tail surfaces, and flying characteristics are provided.
Date: September 1932
Creator: unknown
System: The UNT Digital Library
The Armstrong Whitworth A.W. 16 Military Airplane (British): A Single-Seat Biplane (open access)

The Armstrong Whitworth A.W. 16 Military Airplane (British): A Single-Seat Biplane

Circular presenting a description of the A.W. XVI, which is a single-bay staggered biplane of metal construction with a clean external design. A description of the tail unit, control system, cockpit, fuselage, characteristics, performance, drawings, and photographs are provided.
Date: January 1932
Creator: unknown
System: The UNT Digital Library
The S.A.B.C.A. "S.XI" Commercial Airplane (Belgian): A High-Wing Semicantilever Monoplane (open access)

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

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, characteristics, performances, drawings, and photographs are provided.
Date: April 1932
Creator: Frachet, André
System: The UNT Digital Library
The S.P.C.A. 30 M.4 Military Airplane (French): A Multiplace Low-Wing Airplane (open access)

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, components, engines, characteristics, performance, drawings, and photographs are provided.
Date: September 1932
Creator: unknown
System: The UNT Digital Library
The D.H. "Fox Moth" Commercial Airplane (British): A Three-Passenger Light Cabin Biplane (open access)

The D.H. "Fox Moth" Commercial Airplane (British): A Three-Passenger Light Cabin Biplane

Circular describing the D.H. 83 "Fox Moth", which is a three-passenger light cabin biplane that is considered a commercial airplane despite taking many of its components from the company's existing two-seat touring and training light airplanes. A description of these components, design, flight characteristics, performance, drawings, and photographs are provided.
Date: May 1932
Creator: unknown
System: The UNT Digital Library
Nieuport-Delage 590 Military Airplane (French): A Two-Place High-Wing Cantilever Monoplane (open access)

Nieuport-Delage 590 Military Airplane (French): A Two-Place High-Wing Cantilever Monoplane

Circular presenting a description of the Nieuport-Delage 590 three-engine colonial cantilever monoplane, which meets the requirements of the program established by the French Government. Information is provided regarding the design, construction, and instruments are provided.
Date: November 1932
Creator: unknown
System: The UNT Digital Library
The Avro 631 Training Airplane (British): A Two-Seat Light Biplane (open access)

The Avro 631 Training Airplane (British): A Two-Seat Light Biplane

Circular describing the Avro 631 training airplane, which is a British two-seat light biplane that is meant to be affordable and small. Details regarding the wings, fuselage, tail unit, landing gear, power plant, accommodation, characteristics, performance, drawings, and photographs are provided.
Date: May 1932
Creator: unknown
System: The UNT Digital Library
The Farman Night Bombers 211 and 212 (French): Four-Engine High-Wing Monoplanes (open access)

The Farman Night Bombers 211 and 212 (French): Four-Engine High-Wing Monoplanes

Circular presenting a description of the Farman night bombers 211 and 212, which are four-engine high-wing monoplanes that are equipped with different engines. Details of the wing structure, fuselage, tail surface and controls, landing gear, power plant, characteristics, performance, drawings, and photographs are provided.
Date: July 1932
Creator: unknown
System: The UNT Digital Library
Airplane Flight in the Stratosphere (open access)

Airplane Flight in the Stratosphere

This brief survey of the problems encountered in high-altitude flight deals in particular with the need for high lift coefficient in the wings, large aspect ratios in the wings, and also the problem of hermetically sealing the cabin.
Date: February 1932
Creator: de Caria, Ugo
System: The UNT Digital Library
Problems Concerning the Stability and Maneuverability of Airplanes (open access)

Problems Concerning the Stability and Maneuverability of Airplanes

"The stability of an airplane can be easily determined by wind-tunnel tests, especially by simple tests with models mounted wind-vane fashion. However, each stability curve plotted by this method is valid only for a certain setting of the corresponding control surface, i.e., it characterizes the stability of the airplane with the control stick in a given position. The problems thus defined are studied from the point of view of longitudinal and transverse stability. Directional stability is not included in this study" (p. 1).
Date: March 1932
Creator: Biche, Jean
System: The UNT Digital Library
Accurate Calculation of Multispar Cantilever and Semicantilever Wings With Parallel Webs Under Direct and Indirect Loading (open access)

Accurate Calculation of Multispar Cantilever and Semicantilever Wings With Parallel Webs Under Direct and Indirect Loading

In the present report the computation is actually carried through for the case of parallel spars of equal resistance in bending without direct loading, including plotting of the influence lines; for other cases the method of calculation is explained. The development of large size airplanes can be speeded up by accurate methods of calculation such as this.
Date: March 1932
Creator: Sänger, Eugen
System: The UNT Digital Library
The Mutual Action of Airplane Body and Power Plant (open access)

The Mutual Action of Airplane Body and Power Plant

The present report concerns the development of general propeller performance and r.p.m. curves which, combined with the general curve of the power required for level flight, presents a complete picture of the performance. The curve of power required for level flight in this paper is only an approximation for constant profile drag coefficient, meaning that it is not suitable to unconventional wing sections.
Date: April 1932
Creator: Schrenk, Martin
System: The UNT Digital Library
Spartan "Cruiser" Commercial Airplane (British): A Six-Seat Low-Wing Cantilever Monoplane (open access)

Spartan "Cruiser" Commercial Airplane (British): A Six-Seat Low-Wing Cantilever Monoplane

Circular describing the Spartan "Cruiser", which is a six-seat low-wing cantilever commercial monoplane with three engines. Details of the construction, fuselage, wing, tail unit, power plant, fuel system, lubrication system, landing gear, controls, cabin arrangement, characteristics, performance, drawings, and photographs are provided.
Date: August 1932
Creator: unknown
System: The UNT Digital Library
The Loire 11 Colonial Military Airplane (French): A High-Wing Semicantilever All-Metal Monoplane (open access)

The Loire 11 Colonial Military Airplane (French): A High-Wing Semicantilever All-Metal Monoplane

Circular presenting a description of the Loire 11 military airplane, which is a landplane. Information regarding the materials, wing, fuselage, power plant, flight characteristics, and some photographs are provided.
Date: March 1932
Creator: Loyer, P.
System: The UNT Digital Library
The Breda 32 Commercial Airplane (Italian): A Three-Engine All-Metal Low-Wing Monoplane (open access)

The Breda 32 Commercial Airplane (Italian): A Three-Engine All-Metal Low-Wing Monoplane

Circular presenting a description of the Breda 32, which is a commercial airplane with three engines and an all-metal construction. Details regarding the design, components, flight qualities, drawings, and photographs are provided.
Date: August 1932
Creator: unknown
System: The UNT Digital Library
The Stieger ST. 4 Light Airplane (British): A Twin-Engine Four-Seat Low-Wing Cabin Monoplane (open access)

The Stieger ST. 4 Light Airplane (British): A Twin-Engine Four-Seat Low-Wing Cabin Monoplane

Circular describing the Stieger ST. 4, which is a twin-engine low-wing monoplane of the full cantilever type. Details regarding the wing, fuselage, power plant, landing gear, characteristics, drawings, and photographs are provided.
Date: May 1932
Creator: unknown
System: The UNT Digital Library
The C.A.M.S. 80 Amphibian (French): An Observation Monoplane (open access)

The C.A.M.S. 80 Amphibian (French): An Observation Monoplane

Circular presenting a description of the C.A.M.S. 80, which is a shipboard or observation patrol, light-bombing, long-range amphibian. Details of the hull, landing gear, wing, tail surfaces, power plant, front cockpit, pilot's compartment, photographer's compartment, radio cabinet, rear gunner's cockpit, stern compartment, and flying qualities are provided.
Date: March 1932
Creator: unknown
System: The UNT Digital Library
Properties of Crude Oil From the Greasewood Flat Area in Colorado (open access)

Properties of Crude Oil From the Greasewood Flat Area in Colorado

Report issued by the U.S. Bureau of Mines on two samples of crude oil collected from the Greasewood Flat area of northwestern Colorado. These samples were analyzed for many characteristics, and an approximate summary of those characteristics are presented. The report contains two tables of data.
Date: May 1932
Creator: Rue, H. P.
System: The UNT Digital Library
Migration of Injected Gas Through Oil and Gas Sands of California (open access)

Migration of Injected Gas Through Oil and Gas Sands of California

Report issued by the U.S. Bureau of Mines on the migration of gas injected into reservoir sands. The movements, speed, and direction of the gas are studied. This report includes tables, graphs, and illustrations.
Date: June 1932
Creator: Miller, H. C.
System: The UNT Digital Library
United States Earthquakes, 1930 (open access)

United States Earthquakes, 1930

Report discussing earthquake activity in the United States during 1930. The report is broken down by regions and has sections for specific earthquakes.
Date: 1932
Creator: Neumann, Frank & Bodle, R. R.
System: The UNT Digital Library
United States Earthquakes, 1931 (open access)

United States Earthquakes, 1931

Report discussing earthquake activity in the United States during 1931. The report is broken down by regions and has sections for specific earthquakes.
Date: 1932
Creator: Neumann, Frank
System: The UNT Digital Library
United States Earthquakes, 1932 (open access)

United States Earthquakes, 1932

Report discussing earthquake activity in the United States during 1932. The report is broken down by regions and has sections for specific earthquakes.
Date: 1932
Creator: unknown
System: The UNT Digital Library