Language

Alterations and Tests of The "Farnboro" Engine Indicator (open access)

Alterations and Tests of The "Farnboro" Engine Indicator

"The 'Farnboro' electric indicator was tested as received from the manufacturers, and modifications made to the instrument to improve its operation. The original design of disk valve was altered so as to reduce the mass, travel, and seat area. Changes were made to the recording mechanism, which included a new method of locating the top center position on the record. The effect of friction on the motion of the pointer while taking motoring and power cards was eliminated by providing a means of putting pressure lines on the record" (p. 1).
Date: September 1930
Creator: Collins, John H., Jr.
Object Type: Report
System: The UNT Digital Library
Biennial Report of the Texas Library and Historical Commission State Library: 1928-1930 (open access)

Biennial Report of the Texas Library and Historical Commission State Library: 1928-1930

Biennial report of the Texas Library and Historical Commission for the years 1928-1930, including the budget and summaries of the library's activities.
Date: September 1, 1930
Creator: Texas State Library
Object Type: Report
System: The Portal to Texas History
The Breguet 270 General-Purpose Military Airplane (French): A Two-Seat All-Steel Sesquiplane (open access)

The Breguet 270 General-Purpose Military Airplane (French): A Two-Seat All-Steel Sesquiplane

Circular presenting a description of the Breguet 270 general-purpose military airplane, which is a two-set, all-steel sesquiplane. Details regarding the basic principles of design, construction, components, flying qualities, drawings, and photographs are provided.
Date: September 1930
Creator: De Marolles, R. J.
Object Type: Report
System: The UNT Digital Library
Determination of the Maximum Control Forces and Attainable Quickness in the Operation of Airplane Controls (open access)

Determination of the Maximum Control Forces and Attainable Quickness in the Operation of Airplane Controls

"This report is intended to furnish bases for load assumptions in the designing of airplane controls. The maximum control forces and quickness of operation are determined. The maximum forces for a strong pilot with normal arrangement of the controls is taken as 1.25 times the mean value obtained from tests with twelve persons. Tests with a number of persons were expected to show the maximum forces that a man of average strength can exert on the control stick in operating the elevator and ailerons and also on the rudder bar" (p. 1).
Date: September 1930
Creator: Hertel, Heinrich
Object Type: Report
System: The UNT Digital Library
Effects of the End Fixation of Airplane Struts (open access)

Effects of the End Fixation of Airplane Struts

The main purpose of this report is to give references to literature on the subject of end fixation of airplane struts and also to furnish the constructor with a general survey of the simplest methods for estimating the end-fixation effect.
Date: September 1930
Creator: Teichmann, Alfred
Object Type: Report
System: The UNT Digital Library
Flight Tests for the Determination of Static Longitudinal Stability (open access)

Flight Tests for the Determination of Static Longitudinal Stability

The accuracy of the instruments used for flight test measurements has been inadequate so a new series of tests were commissioned with the development of an accurate elevator setting recorder.
Date: September 1930
Creator: Blenk, Hermann
Object Type: Report
System: The UNT Digital Library
Game laws for the season 1930-31 : a summary of federal, state, and provincial statutes. (open access)

Game laws for the season 1930-31 : a summary of federal, state, and provincial statutes.

Describes laws and regulations for hunting and fishing in North America.
Date: September 1930
Creator: Earnshaw, Frank L. & Grimes, Frank G.
Object Type: Book
System: The UNT Digital Library
The Henderson "Hendy" 302 Cabin Airplane (British): A Two-Seat Low-Wing Cantilever Monoplane (open access)

The Henderson "Hendy" 302 Cabin Airplane (British): A Two-Seat Low-Wing Cantilever Monoplane

Circular presenting a description of the Hendy 302, which is a two-seat, low-wing cantilever monoplane with a hinged cabin top. A description of the design, flying qualities, and photographs are provided.
Date: September 1930
Creator: unknown
Object Type: Report
System: The UNT Digital Library
An Investigation of Airplane Landing Speeds (open access)

An Investigation of Airplane Landing Speeds

"This paper describes an investigation on airplane landing speeds which was made to determine the applicability of accepted aerodynamic theory to the prediction of this particular performance characteristic. The experimental work consisted in measuring the landing speed of several monoplanes by a new photographic method. The results of these tests supplemented by available information regarding biplanes were compared with predictions made with basic aerodynamic theory" (p. 1).
Date: September 1930
Creator: Ridley, Kenneth F.
Object Type: Report
System: The UNT Digital Library
List of State Registered Plant Breeders and State Certified Seed Growers Licensed to Produce State Registered and State Certified Planting Seed for the Year 1930 (open access)

List of State Registered Plant Breeders and State Certified Seed Growers Licensed to Produce State Registered and State Certified Planting Seed for the Year 1930

Document outlining information related to the Texas Field Seed Certification Law, including information about varieties as well as field inspections and other regulatory information.
Date: September 1930
Creator: Humbert, E. P.; Del Curto, J. M. & Farris, W. D.
Object Type: Pamphlet
System: The Portal to Texas History
Load Assumptions for Calculating the Strength of Airplanes (open access)

Load Assumptions for Calculating the Strength of Airplanes

"The following load assumptions shall be taken as the basis of the strength calculations. Certain definite load conditions (e.g. of flight, control, landing and transport) shall be assumed. The loads shall be assumed to be safe loads, constant or only slowly variable, and the inertia forces due to elastic deformation are accordingly disregarded. The external forces, the force of gravity and the inertia forces on the whole airplane shall produce a condition of equilibrium" (p. 1).
Date: September 1930
Creator: unknown
Object Type: Report
System: The UNT Digital Library
Why Some Wood Surfaces Hold Paint Longer Than Others. (open access)

Why Some Wood Surfaces Hold Paint Longer Than Others.

Describes the different factors to consider when selecting wood to be painted.
Date: September 1930
Creator: Browne, F. L. (Frederick Lincoln), 1895-
Object Type: Book
System: The UNT Digital Library
Coefficients of discharge of fuel-injection nozzles for compression-ignition engines (open access)

Coefficients of discharge of fuel-injection nozzles for compression-ignition engines

"This report presents the results of an investigation to determine the coefficients of discharge of nozzles with small, round orifices of the size used with high-speed compression-ignition engines. The injection pressures and chamber back pressures employed were comparable to those existing in compression-ignition engines during injection. The construction of the nozzles was varied to determine the effect of the nozzle design on the coefficient. Tests were also made with nozzles assembled in an automatic injection valve, both with a plain and with a helically grooved stem" (p. 193).
Date: September 11, 1930
Creator: Gelalles, A. G.
Object Type: Report
System: The UNT Digital Library
Some approximate equations for the standard atmosphere (open access)

Some approximate equations for the standard atmosphere

This report contains the derivation of a series of simple approximate equations for density ratios and for the pressure ratio in the standard atmosphere. The accuracy of the various equations is discussed and the limits of applications are given. Several of these equations are in excellent agreement with the standard values.
Date: September 19, 1930
Creator: Diehl, Walter S.
Object Type: Report
System: The UNT Digital Library
Breguet Military Airplane, Type 33: A Two-Place Long-Distance Sesquiplane for Observation and Bombing (open access)

Breguet Military Airplane, Type 33: A Two-Place Long-Distance Sesquiplane for Observation and Bombing

Circular presenting a description of the Breguet military airplane, Type 33, which is a two-place long-distance sesquiplane made for observation and bombing. Details of the components, bomb dropping, flying qualities, design, flying qualities and performances, drawings, and photographs are provided.
Date: September 1931
Creator: unknown
Object Type: Report
System: The UNT Digital Library
The Dangerous Sideslip of a Stalled Airplane and Its Prevention (open access)

The Dangerous Sideslip of a Stalled Airplane and Its Prevention

This investigation covers only that phase of airplane accidents which are the result of sideslip. We examine the circumstances under which this occurs, study the behavior of present-day airplane types (monoplane, conventional and staggered biplane) therein and endeavor to find a solution whereby this danger may be avoided.
Date: September 1931
Creator: Fuchs, Richard & Schmidt, Wilhelm
Object Type: Report
System: The UNT Digital Library
The development, design and construction of gliders and sailplanes (open access)

The development, design and construction of gliders and sailplanes

This report explains and details the history of glider design and construction through the impetus of the Rhon Sailplane contests. Some of the topics considered include: whether the longitudinal stability (dynamic and static) is sufficient in the tailless typo and a consideration that the structural weight of sweptback wings would be greater than that of a corresponding normal wing.
Date: September 1931
Creator: Lippisch, A.
Object Type: Report
System: The UNT Digital Library
Experiments With Airplane Brakes (open access)

Experiments With Airplane Brakes

This report begins by examining the forces on the brake shoes. For the determination of the load distribution over the shoes it was assumed that the brake linings follow Hooke's law, are neatly fitted and bedded in by wear. The assumption of Hooke's law, that is, the proportionality between compression of the lining and the absorption of force, is fulfilled to a certain extent for the loading, as becomes apparent from the load tests described further on. But there is a material discrepancy at unloading.
Date: September 1931
Creator: Michael, Franz
Object Type: Report
System: The UNT Digital Library
Full Text of the Game, Fish, and Oyster Laws of Texas, September 1931 (open access)

Full Text of the Game, Fish, and Oyster Laws of Texas, September 1931

Text of laws governing fishing and oyster culture, as well as regulation by the Game, Fish, and Oyster Commission. Index starts on page 159.
Date: September 1, 1931
Creator: Texas. Game, Fish, and Oyster Commission.
Object Type: Book
System: The Portal to Texas History
An Investigation of Cotton for Parachute Cloth (open access)

An Investigation of Cotton for Parachute Cloth

"This is a resume of the work of the Bureau of Standards on a cotton parachute cloth for use as a substitute for silk in the event of an emergency curtailing the supply. Cotton yarn of high strength in proportion to its weight and otherwise specially suitable for parachute cloth was developed. Cloth woven from this yarn in the bureau mill was equal or superior to parachute silk in strength and tear resistance, met the requirements with respect to air permeability, and weighed only a few tenths of an ounce per square yard more than the silk cloth" (p. 1).
Date: September 1931
Creator: Appel, William D. & Worner, R. K.
Object Type: Report
System: The UNT Digital Library
List of State Registered Plant Breeders and State Certified Seed Growers Licensed to Produce State Registered and State Certified Planting Seed for the Year 1931. (open access)

List of State Registered Plant Breeders and State Certified Seed Growers Licensed to Produce State Registered and State Certified Planting Seed for the Year 1931.

Agriculture bulletin that list plant breeders and seed growers that are registered by the state. This bulletin also includes a license to produce state registered and certified planting seeds for the year 1931.
Date: September 1931
Creator: Texas. State Seed and Plant Board.
Object Type: Pamphlet
System: The Portal to Texas History
A method for reducing the temperature of exhaust manifolds (open access)

A method for reducing the temperature of exhaust manifolds

From Summary: "This report describes tests conducted at the Langley Memorial Aeronautical Laboratory on an "air-inducting" exhaust manifold for aircraft engines. The exhaust gases from each cylinder port are discharged into the throat of an exhaust pipe which has a frontal bellmouth. Cooling air is drawn into the pipe, where it surrounds and mixes with the exhaust gases. Temperatures of the manifold shell and of the exhaust gases were obtained in flight for both a conventional manifold and the air-inducting manifold."
Date: September 1931
Creator: Schey, Oscar W. & Young, Alfred W.
Object Type: Report
System: The UNT Digital Library
The N.A.C.A. Apparatus for Studying the Formation and Combustion of Fuel Sprays and the Results From Preliminary Tests (open access)

The N.A.C.A. Apparatus for Studying the Formation and Combustion of Fuel Sprays and the Results From Preliminary Tests

Described here is an apparatus for studying the formation and combustion of fuel sprays under conditions closely simulating those in a high speed compression-ignition engine. The apparatus consists of a single-cylinder modified test engine, a fuel injection system so designed that a single charge of fuel can be injected into the combustion chamber, an electric driving motor, and a high-speed photographic apparatus. When the fuel is injected into the combustion chamber, motion pictures at the rate of 2000 per second are taken of the spray formation by means of spark discharges.
Date: September 1931
Creator: Rothrock, A. M.
Object Type: Report
System: The UNT Digital Library
On Floats and Float Tests (open access)

On Floats and Float Tests

The principal source of information on float resistance is the model test. In view of the insuperable difficulties opposing any attempt at theoretical treatment of the resistance problem, particularly at attitudes which tend toward satisfactory take-off, such as the transitory stage to planing, the towing test is and will remain the primary method for some time.
Date: September 1931
Creator: Seewald, Friedrich
Object Type: Report
System: The UNT Digital Library