Diehl, Walter S. (Walter Stuart), 1893-1976
Diehl, Walter S.
Diehl, Walter S. (Walter Stuart)
Walter Stuart Diehl American aeronautical engineer
Diehl, Walter Stuart, 1893-1976
VIAF ID: 118511262 ( Personal )
Permalink: http://viaf.org/viaf/118511262
Preferred Forms
- 100 1 _ ‡a Diehl, Walter S.
- 100 1 _ ‡a Diehl, Walter S. ‡q (Walter Stuart)
-
- 100 1 _ ‡a Diehl, Walter S. ‡q (Walter Stuart), ‡d 1893-1976
- 100 1 _ ‡a Diehl, Walter Stuart, ‡d 1893-1976
- 100 0 _ ‡a Walter Stuart Diehl ‡c American aeronautical engineer
4xx's: Alternate Name Forms (6)
Works
Title | Sources |
---|---|
The air forces on a model of the Sperry Messenger airplane without propeller | |
The application of basic data on planing surfaces to the design of flying-boat hulls | |
The application of propeller test data to design and performance caluclations | |
Balloon and airship gases. | |
The calculation of take-off run | |
A discussion of certain problems connected with the design of hulls of flying boats and the use of general test data | |
The effect of flight path inclination on private velocity | |
Engine performance and the determination of absolute ceiling | |
Engineering aerodynamics. | |
The estimation of maximum load capacity of seaplanes and flying boats | |
The general efficiency curve for air propellers | |
Joint report on standardization tests on N. P. L. R. A. F. 15 airfoil model | |
The mean aerodynamic chord and the aerodynamic center of a tapered wing | |
A new chart for estimating the absolute ceiling of an airiplane | |
no99017803 | |
The reduction of observed airplane performance to standard conditions | |
Relative efficiency of direct and geared drive propellers | |
Relative loading on biplane wings of unequal chords | |
Reliable formulæ for estimating airplane performance and the effects of changes in weight, wing area, or power | |
Some approximate equations for the standard atmosphere | |
Standard atmosphere-tables and data | |
Static thrust of airplane propellers | |
A study of the effect of a diving start on airplane speed... Reprint... | |
Tests on airplane fuselages, floats and hulls | |
Tests on models of three British airplanes in the variable density wind tunnel | |
Three methods of calculating range and endurance of airplanes | |
Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane. | |
The variation of aerofoil lift and drag coefficients with changes in size and speed. |