Add to ORKGTests were made in the no. 1 wind tunnel at Langley Memorial Aeronautical Laboratory to determine the air forces acting on rotating cylinders with axes perpendicular to the direction of motion. One cylinder had a circular cross-section, the other that of a greek cross
The tests, conducted at the Guggenheim Aeronautical Laboratory of Stanford University, to investigat...
Experiments were performed to determine the power required for rotating a rotor disc fitted with a n...
Test of 10-foot diameter, four and six blade single-rotating and dual-rotating propellers were condu...
Into the leading edge of a wing with arbitrary cross-section, there is introduced a cylinder, which ...
Steady rotational oscillations of circular cylinder in the air stream are studied experimentally. Cy...
In the closer investigation of the results obtained from a wing model with a rotary cylinder mounted...
Two rotary balance apparatuses were developed for testing airplane models in a coning motion. A larg...
With the assistance and cooperation of the National Advisory Committee for Aeronautics the Bureau of...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1916.by Tsa...
Tests have been made at high speeds to determine the drag of models, simulating propeller shanks, in...
This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were...
Rotational and translational oscillations of three cylinders differing in the ratio of length to cy...
This is the thirteenth report on a series of systematic tests comparing lateral control devices with...
Report presents the results of a study made to determine the air-flow characteristics around finned ...
This lecture deals with four main subjects: methods of studying air resistance, experimental aerodyn...
The tests, conducted at the Guggenheim Aeronautical Laboratory of Stanford University, to investigat...
Experiments were performed to determine the power required for rotating a rotor disc fitted with a n...
Test of 10-foot diameter, four and six blade single-rotating and dual-rotating propellers were condu...
Into the leading edge of a wing with arbitrary cross-section, there is introduced a cylinder, which ...
Steady rotational oscillations of circular cylinder in the air stream are studied experimentally. Cy...
In the closer investigation of the results obtained from a wing model with a rotary cylinder mounted...
Two rotary balance apparatuses were developed for testing airplane models in a coning motion. A larg...
With the assistance and cooperation of the National Advisory Committee for Aeronautics the Bureau of...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1916.by Tsa...
Tests have been made at high speeds to determine the drag of models, simulating propeller shanks, in...
This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were...
Rotational and translational oscillations of three cylinders differing in the ratio of length to cy...
This is the thirteenth report on a series of systematic tests comparing lateral control devices with...
Report presents the results of a study made to determine the air-flow characteristics around finned ...
This lecture deals with four main subjects: methods of studying air resistance, experimental aerodyn...
The tests, conducted at the Guggenheim Aeronautical Laboratory of Stanford University, to investigat...
Experiments were performed to determine the power required for rotating a rotor disc fitted with a n...
Test of 10-foot diameter, four and six blade single-rotating and dual-rotating propellers were condu...