Author: Air Corps / Publisher: Engineering Division - Blacklight Search Results

Start Over Author Air Corps Publisher Engineering Division

1. Beacons. Twenty-four inch revolving incandescent beacon, Air Corps type B-3, Equipment Section report; by W. T. Harding.

Corporate/Agency Authors:: Engineering Division, Air Corps, and War Department
Publisher:: Engineering Division
Date:: 1926
SuDoc number:: W 87.11/2:6/574

2. Carbureters. Development and test of Stromberg NA-Y5D carburetor for Curtiss D-12 engine, Power Plant Section report; by J. M. Miller.

Corporate/Agency Authors:: Engineering Division, Air Corps, and War Department
Publisher:: Engineering Division
Date:: 1926
SuDoc number:: W 87.11/2:6/572

3. Carbureters. Development and test of Zenith ED-52 carburetor for liberty 12 engine, Power Plant Section report; by J. M. Miller.

Corporate/Agency Authors:: Engineering Division, Air Corps, and War Department
Publisher:: Engineering Division
Date:: 1926
SuDoc number:: W 87.11/2:6/570

4. Carburetor metering jet calibration, Power Plant Section; by Opie Chenoweth.

Corporate/Agency Authors:: Engineering Division, Air Corps, and War Department
Publisher:: Engineering Division
Date:: 1926
SuDoc number:: W 87.11/2:6/569

5. Flood lights. Comparative flood-light test, Equipment Section report; by D. L. Bruner and W. T. Harding.

Corporate/Agency Authors:: Engineering Division, Air Corps, and War Department
Publisher:: Engineering Division
Date:: 1926
SuDoc number:: W 87.11/2:6/571

6. Stresses. Critical loading of structural members subjected to combined axial and transverse loads. Airplane Section report; by J. E. Younger.

Corporate/Agency Authors:: Engineering Division, Air Corps, and War Department
Publisher:: Engineering Division
Date:: 1926
SuDoc number:: W 87.11/2:6/581

7. Struts. Strength of bent struts, Airplane Section report; by J. E. Younger.

Corporate/Agency Authors:: Engineering Division, Air Corps, and War Department
Publisher:: Engineering Division
Date:: 1926
SuDoc number:: W 87.11/2:6/580

8. Wind tunnel test of Clark Y, Clark Y-15, Clark Y-18, Clark Y-21, Gottingen 398, and S. T. Ae'-27a, 6″X36″ airfoils, tests nos. 233, 234, and 237, Airplane Section report; prepared by Aerodynamics Branch.

Corporate/Agency Authors:: Engineering Division, Air Corps, and War Department
Publisher:: Engineering Division
Date:: 1926
SuDoc number:: W 87.11/2:6/573