Resource Type
Partner
Collection
Technical Report Archive and Image Library
195
National Advisory Committee for Aeronautics Collection
165
Boy and Girl Scout Annual Reports
1
Dallas Park and Recreation Department Photographs
1
Oklahoma Historical Society Manuscript Collection
1
Rescuing Texas History, 2010
1
Government Documents General Collection
1
Serial/Series Title
NACA Technical Memorandums
67
NACA Technical Notes
51
NACA Technical Reports
45
United States Bureau of Mines Reports
26
Bulletin (United States. Bureau of Mines)
5
Report of investigations (United States. Bureau of Mines)
5
Technical paper (United States. Bureau of Mines)
5
NACA Annual Reports
2
National Bureau of Standards Reports
2
Annual Report of the Boy Scouts of America
1
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Results:
193 - 199 of
199
Control in Circling Flight
"This investigation was undertaken for the purpose of developing instruments that would record the forces and positions of all three controls, and to obtain data on the behavior of an airplane in turns. All the work was done on a standard rigged JN4H (airplane no. 2 of National Advisory Committee for Aeronautics, report no. 70). It was found that the airplane was longitudinally unstable and nose heavy; that it was laterally unstable, probably due to too little dihedral; and that it was directionally unstable, due to insufficient fin area, this last being very serious, for in case of a loss of rudder control the airplane immediately whips into a spin from which there is no way of getting it out" (p. 71).
Date:
1923
Creator:
Norton, F. H. & Allen, E. T.
System:
The UNT Digital Library
Some New Aerodynamical Relations
This report contains three new relations extending the modern theory of aeronautics. The first part contains a relation between the power absorbed by an aerofoil and the power absorbed by a propeller. In the second part the exactness of the ordinary formula for the induced drag of an aerofoil is examined and the error is determined. In the third part the author shows that for the calculation of the air forces on bodies of considerable volume the imaginary sources and sinks equivalent to the flow around the body can be used in the same way as vortices are used for the calculation of lift and induced drag of wings.
Date:
1923
Creator:
Munk, Max M.
System:
The UNT Digital Library
Controllability and Maneuverability of Airplanes
This investigation was conducted for the purpose of studying the behavior of the JN4H airplane in free flight under the action of its controls and from this to arrive at satisfactory definitions and coefficients for controllability and maneuverability. The method consisted in recording the angular velocity about the three axes, together with the air speed, control positions, and acceleration.
Date:
1923
Creator:
Norton, F. H. & Brown, W. G.
System:
The UNT Digital Library
Annual Report of the Marland Oil Company and Subsidiary Companies
Annual report of the Marland Oil Company showing assets, liabilities, stocks, and and income statement.
Date:
1923
Creator:
unknown
System:
The Gateway to Oklahoma History
The Air Propeller, Its Strength and Correct Shape
It is possible to give a propeller such a shape that, under given conditions, viz., a definite speed of revolution and flying speed, the bending stresses in the blades will assume quite an insignificant magnitude.
Date:
February 1923
Creator:
Dietsius, H.
System:
The UNT Digital Library
Report on the Oil and Gas Possibilities of the University Block 46 in Culberson County
Report that discusses the oil and gas possibilities in Culberson County, Texas. The geology of the area is discussed and divided into two sections.
Date:
December 8, 1923
Creator:
Beede, J. W., 1871-1940
System:
The UNT Digital Library
Annual Report of the Boy Scouts of America: 1922
Annual report submitted by the Boy Scouts of America to Congress describing highlights from 1922, activities, finance, organizational leadership, and other information about scouting programs.
Date:
April 1, 1923
Creator:
Boy Scouts of America
System:
The Portal to Texas History