A test was conducted in the Arnold Engineering Development Center (AEDC) Aerodynamic Wind Tunnel (1T) of the Propulsion Wind Tunnel Facility (PWT) to measure the flow fields about several wing/pylon/store configurations. Test models included a wall-mounted swept wing, five-percent MK-83 and M-117 stores, and swept and unswept pylons. Flow-field velocity measurements, made by using a three-component laser velocimeter, are presented. (Author).Report was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc."Final Report: March 8, 1978 -- September 30, 1980.""August 1981."Includes bibliograqphic references (pages 11-12).A test was conducted in the Arnold Engineering Development Center (AEDC) Aerodynamic Wind Tunnel (1T) ...
An investigation was conducted in the Langley V/STOL tunnel with a laser velocimeter to obtain measu...
Tests were conducted on a four-finned, ogive-cylinder store model which was mounted on the von Karma...
Laser anemometer surveys were made of the 3-D flow field in NASA rotor 67, a low aspect ratio transo...
Tests were conducted in the VKF/A and PWT/4T wind tunnels at AEDC to obtain captive trajectory, aero...
Experimental data were obtained to aid in the prediction of aerodynamic loads and separation-traject...
The need for measurements of the velocity flow field about spinner propeller nacelle configurations ...
A wind-tunnel investigation was carried out on an oscillating model of the F-5 wing with and without...
Off-body flow visualizations and fluid velocity measurements are conducted in a supersonic vortex fl...
This test was conducted in support of a program to develop a generalized analytical method for predi...
This paper illustrates of instantaneous flow field measurements which were performed by the PIV grou...
The paper illustrates results of instantaneous flow field measurements which were performed by the P...
A new measurement technique is being developed by NASA to measure off-surface flow fields. This meth...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
The experimental investigation of unsteady complex flow fields in wind tunnels requires advanced mea...
A new measurement technique is being developed by NASA to measure off-surface flow fields. This meth...
An investigation was conducted in the Langley V/STOL tunnel with a laser velocimeter to obtain measu...
Tests were conducted on a four-finned, ogive-cylinder store model which was mounted on the von Karma...
Laser anemometer surveys were made of the 3-D flow field in NASA rotor 67, a low aspect ratio transo...
Tests were conducted in the VKF/A and PWT/4T wind tunnels at AEDC to obtain captive trajectory, aero...
Experimental data were obtained to aid in the prediction of aerodynamic loads and separation-traject...
The need for measurements of the velocity flow field about spinner propeller nacelle configurations ...
A wind-tunnel investigation was carried out on an oscillating model of the F-5 wing with and without...
Off-body flow visualizations and fluid velocity measurements are conducted in a supersonic vortex fl...
This test was conducted in support of a program to develop a generalized analytical method for predi...
This paper illustrates of instantaneous flow field measurements which were performed by the PIV grou...
The paper illustrates results of instantaneous flow field measurements which were performed by the P...
A new measurement technique is being developed by NASA to measure off-surface flow fields. This meth...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
The experimental investigation of unsteady complex flow fields in wind tunnels requires advanced mea...
A new measurement technique is being developed by NASA to measure off-surface flow fields. This meth...
An investigation was conducted in the Langley V/STOL tunnel with a laser velocimeter to obtain measu...
Tests were conducted on a four-finned, ogive-cylinder store model which was mounted on the von Karma...
Laser anemometer surveys were made of the 3-D flow field in NASA rotor 67, a low aspect ratio transo...