Add to ORKGThe Langley 16-foot transonic wind tunnel is described. The system configuration, optical layout, laser color separator, optical receiver, and tunnel window are discussed
A large wind tunnel, approximately 8 feet in diameter, has been converted to transonic operation by ...
The Langley 6 by 28 inch transonic tunnel is described. The tunnel is a two dimensional facility wit...
Prepared at Langley Research Center and Aerostructures Diectorate, USAARTA-AVSCOM."December 1985"--C...
The need for measurements of the velocity flow field about spinner propeller nacelle configurations ...
The Langley 16-Foot Transonic Tunnel is a single-return, continuous-flow, atmospheric tunnel which u...
The operational characteristics and equipment associated with the Langley 16-foot transonic tunnel c...
The Langley 16 x 24 inch Water Tunnel is described in detail, along with all the supporting equipmen...
The problems and the potential use of a nonintrusive flow velocity measuring technique in the Langle...
The Laser Transit Anemometer (LTA) system is described. In the LTA system two parallel laser beams o...
A unique laser velocimeter was developed that is capable of sensing two orthogonal velocity componen...
A long-focal length laser velocimeter constructed in the early 1980's was upgraded using current tec...
Femtosecond laser electronic excitation and tagging (FLEET) velocimetry is demonstrated in a large-s...
Three seeding systems have been used in the 4- by 7- Meter Tunnel at NASA Langley Research Center: K...
Laser probe using Doppler shift of scattered laser light for high temperature wind tunnel velocity m...
The historical development of laser velocimetry and its application to low-speed (less than 100 m/se...
A large wind tunnel, approximately 8 feet in diameter, has been converted to transonic operation by ...
The Langley 6 by 28 inch transonic tunnel is described. The tunnel is a two dimensional facility wit...
Prepared at Langley Research Center and Aerostructures Diectorate, USAARTA-AVSCOM."December 1985"--C...
The need for measurements of the velocity flow field about spinner propeller nacelle configurations ...
The Langley 16-Foot Transonic Tunnel is a single-return, continuous-flow, atmospheric tunnel which u...
The operational characteristics and equipment associated with the Langley 16-foot transonic tunnel c...
The Langley 16 x 24 inch Water Tunnel is described in detail, along with all the supporting equipmen...
The problems and the potential use of a nonintrusive flow velocity measuring technique in the Langle...
The Laser Transit Anemometer (LTA) system is described. In the LTA system two parallel laser beams o...
A unique laser velocimeter was developed that is capable of sensing two orthogonal velocity componen...
A long-focal length laser velocimeter constructed in the early 1980's was upgraded using current tec...
Femtosecond laser electronic excitation and tagging (FLEET) velocimetry is demonstrated in a large-s...
Three seeding systems have been used in the 4- by 7- Meter Tunnel at NASA Langley Research Center: K...
Laser probe using Doppler shift of scattered laser light for high temperature wind tunnel velocity m...
The historical development of laser velocimetry and its application to low-speed (less than 100 m/se...
A large wind tunnel, approximately 8 feet in diameter, has been converted to transonic operation by ...
The Langley 6 by 28 inch transonic tunnel is described. The tunnel is a two dimensional facility wit...
Prepared at Langley Research Center and Aerostructures Diectorate, USAARTA-AVSCOM."December 1985"--C...