Add to ORKGTo furnish data for the design of the fleet airship Shenandoah, a model was made and tested in the 8 by 8 foot wind tunnel for wind forces, moments, and damping, under conditions described in this report. The results are given for air of standard density. P=0.00237 slugs per cubic foot with vl/v correction, and with but a brief discussion of the aerodynamic design features of the airship
This report presents the results of measurements of flow in the boundary layer of a 1/40-scale model...
This report combines the wind tunnel results of tests on four control surface models made in the two...
This investigation was made for the purpose of determining the aerodynamic pressure distribution enc...
This report presents the results of wind tunnel tests conducted to determine the aerodynamic charact...
To furnish data for the design of the fleet airship Shenandoah, a model was made and tested in the 8...
This report presents the results of wind-tunnel tests on eight C-class airship hulls with various fi...
The tests described in this report furnished data on the actual aerodynamic forces, and the resultin...
This report presents the results of full-scale wind tunnel tests conducted to determine the ground-h...
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
The design of complicated structures often presents problems of extreme difficulty which are frequen...
A simple aerodynamic bending moment envelope is derived for conventionally shaped airships. This cri...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
In the text are derived simple formulae for determining, directly from the data of wind tunnel tests...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1932.Microf...
This report describes the new method for making computations in connection with the study of rigid a...
This report presents the results of measurements of flow in the boundary layer of a 1/40-scale model...
This report combines the wind tunnel results of tests on four control surface models made in the two...
This investigation was made for the purpose of determining the aerodynamic pressure distribution enc...
This report presents the results of wind tunnel tests conducted to determine the aerodynamic charact...
To furnish data for the design of the fleet airship Shenandoah, a model was made and tested in the 8...
This report presents the results of wind-tunnel tests on eight C-class airship hulls with various fi...
The tests described in this report furnished data on the actual aerodynamic forces, and the resultin...
This report presents the results of full-scale wind tunnel tests conducted to determine the ground-h...
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
The design of complicated structures often presents problems of extreme difficulty which are frequen...
A simple aerodynamic bending moment envelope is derived for conventionally shaped airships. This cri...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
In the text are derived simple formulae for determining, directly from the data of wind tunnel tests...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1932.Microf...
This report describes the new method for making computations in connection with the study of rigid a...
This report presents the results of measurements of flow in the boundary layer of a 1/40-scale model...
This report combines the wind tunnel results of tests on four control surface models made in the two...
This investigation was made for the purpose of determining the aerodynamic pressure distribution enc...