The results of a series of flow quality and performance tests on several inlet and exit configurations for nonreturn wind tunnels are presented. Test section flow angularities, local dynamic pressure variations, and total-pressure-loss variations are presented as functions of wind-to-test-section dynamic pressure ratio. The results show that a nonreturn wind tunnel should have end treatments with three characteristics: (1) a vertical exit system, (2) a horizontal inlet system, and (3) an area of protected enclosure at the inlet. Inlet and exhaust treatments were developed that produced good aerodynamic flow qualities with low power penalties
Two turning vane designs were experimentally evaluated for corner 2 of a 0.1 scale model of the NASA...
The design and testing of vane sets and air-exchange inlet for the 40 x 80/80 x 120-ft wind tunnel a...
Detailed flow surveys downstream of the corner turning vanes and downstream of the fan inlet guide v...
The study to develop inlet and exit treatments which would minimize the effect of external wind on t...
The refinement of inlet and exit treatments were studied which would minimize the effect of external...
The effect of the external wind on the quality of the flow in the test section was studied. The flow...
The structural cost of non-return wind tunnels is significantly less than that of the more conventio...
The effect of a transient wind on the test-section flow quality of an open-circuit wind tunnel was i...
Low-contraction ratio wind tunnel inlets have been shown to generate nonuniform velocity fields in t...
A series of wind tunnel investigations were conducted to determine the flow characteristics downstre...
General guidelines are given for the design of diffusers, contractions, corners, and the inlets and ...
The present inlet design concept for an indraft wind tunnel, which is especially suited to applicati...
A series of studies were conducted to determine the existing flow quality in the NASA Lewis 8 by 6 F...
Testing of aerodynamic loads on a sub-scale model has been the most accurate way to predict full-sca...
Testing of aerodynamic loads on a sub-scale model has been the most accurate way to predict full-sca...
Two turning vane designs were experimentally evaluated for corner 2 of a 0.1 scale model of the NASA...
The design and testing of vane sets and air-exchange inlet for the 40 x 80/80 x 120-ft wind tunnel a...
Detailed flow surveys downstream of the corner turning vanes and downstream of the fan inlet guide v...
The study to develop inlet and exit treatments which would minimize the effect of external wind on t...
The refinement of inlet and exit treatments were studied which would minimize the effect of external...
The effect of the external wind on the quality of the flow in the test section was studied. The flow...
The structural cost of non-return wind tunnels is significantly less than that of the more conventio...
The effect of a transient wind on the test-section flow quality of an open-circuit wind tunnel was i...
Low-contraction ratio wind tunnel inlets have been shown to generate nonuniform velocity fields in t...
A series of wind tunnel investigations were conducted to determine the flow characteristics downstre...
General guidelines are given for the design of diffusers, contractions, corners, and the inlets and ...
The present inlet design concept for an indraft wind tunnel, which is especially suited to applicati...
A series of studies were conducted to determine the existing flow quality in the NASA Lewis 8 by 6 F...
Testing of aerodynamic loads on a sub-scale model has been the most accurate way to predict full-sca...
Testing of aerodynamic loads on a sub-scale model has been the most accurate way to predict full-sca...
Two turning vane designs were experimentally evaluated for corner 2 of a 0.1 scale model of the NASA...
The design and testing of vane sets and air-exchange inlet for the 40 x 80/80 x 120-ft wind tunnel a...
Detailed flow surveys downstream of the corner turning vanes and downstream of the fan inlet guide v...