与 «VARIABLE-DENSITY WIND TUNNEL»相关的英语书籍
在以下的参考文献中发现
variable-density wind tunnel的用法。与
variable-density wind tunnel相关的书籍以及同一来源的简短摘要提供其在 英语文献中的使用情境。
1
Theory of Wing Sections, Including a Summary of Airfoil Data
Jacobs, Eastman N., and Pinkerton, Robert M.: Tests in the Variable-density Wind
Tunnel of Related Airfoils Having the Maximum Camber Unusually Far Forward.
NACA Rept. No. 537, 1935. 47. Jacobs, Eastman N., and Pinkerton, Robert M.: ...
2
Tests of Six Symmetrical Airfoils in the
Variable Density ...
It gives in preliminary form the results obtained fom tests in the N.A.C.A. variable density wind tunnel of six symmetrical airfoils, differing only in maximum thickness.
Eastman Nixon Jacobs, 1931
3
Applied and Computational Fluid Mechanics
Variable Density Wind Tunnel New 8' 7' 15' 5' 5' 8' 34'–6'' Old FIGURE 6.41
Schematic of the NACA Variable Density Wind Tunnel. Courtesy of NASA. The
NACA Variable Density Tunnel (VDT) (Figure 6.41), built at the Langley
Laboratory in ...
4
The
Wind and Beyond: A Documentary Journey Into the History ...
I note that you do not at present plan to publish this report, and agree that the
difference in drag shown in the results from our variable-density wind tunnel
appears at first a little disturbing. I note however, that you conclude in general
that your ...
James R. Hansen, National Aeronautics and Space Administration, 2009
5
Theory of Wing Sections: Including a Summary of Airfoil Data
Jacobs, Eastman N., and Pinkerton, Robert M.: Tests in the Variable-density Wind
Tunnel of Related Airfoils Having the Maximum Camber Unusually Far Forward.
NACA Rept. No. 537, 1935. 47. Jacobs, Eastman N., and Pinkerton, Robert M.: ...
Ira H. Abbott, A. E. von Doenhoff, 2012
6
Sphere Drag Tests in the
Variable Density Wind Tunnel
The conclusions are that approximately the same drag coefficient is obtained at a given value of the Reynolds number irrespective of what combination of the variables is used to obtain the value of the Reynolds number and that the ...
Eastman Nixon Jacobs, 1929
E. N. Jacobs, J. Stack, and R. M. Pinkerton: "Airfoil Pressure Distribution
Investigation in the Variable Density Wind Tunnel", N.A.C.A. Report No. 353.
Architect's Bookshelf Continued from page 1 1 floors. The outer walls are
conceived as mere ...
8
One Small Step: The History of Aerospace Engineering at ...
In the spring of 1947, Professor Weske learned of a Japanese variable- density
wind tunnel that the Air Forces had confiscated when U.S. military forces
occupied Tokyo. This tunnel was rather advanced because of its variable-density
...
A. F. Grandt, Jr., W. A. Gustafson, L. T. Cargnino, 2010
An exact copy of the National Physical Laboratory airship model is undergoing
test in the variable-density wind tunnel of the committee for comparison of the
results with those obtained in the wind tunnels of the atmospheric type. During
the ...
United States. National Bureau of Standards, 1927
10
1000 Solved Problems in Fluid Mechanics (includes Hydraulic ...
(Ans. Vm =139 m/s, Fp = 42.1 N) Characteristics of a small underwater craft are
studied under dynamic similarity conditions in a variable density wind tunnel on a
model scale of 1 : 12. What prototype speed and power are indicated by model ...
