The NASA Langley Research Center (LaRC) has been engaged in an effort to reduce wind tunnel test cycle time in support of Agency goals and to satisfy the wind tunnel testing needs of the commercial and military aerospace communities. LaRC has established the Wind Tunnel Enterprise (WTE), with goals of reducing wind tunnel test cycle time by an order of magnitude by 2002, and by two orders of magnitude by 2010. The WTE also plans to meet customer expectations for schedule integrity, as well as data accuracy and quality assurance. The WTE has made progress towards these goals over the last year with a focused effort on technological developments balanced by attention to process improvements. This paper presents a summary of several of the WTE...
Large aeronautical ground test facilities, particularly continuous flow wind tunnels and engine alti...
The 7 by 10 foot high speed tunnel performs a wide range of tests employing a variety of model insta...
This paper describes the results of two recent process improvements; drag feed-forward Mach number c...
The advantage of managing organizations to minimize product development cycle time has been well est...
After 4 years of existence, the Langley WTE is alive and growing. Significant improvements in the op...
Enhancing wind tunnel test productivity in terms of increased efficiency, reduced cost, and expanded...
Productivity gains have recently been made at the National Transonic Facility wind tunnel at NASA La...
Description, capabilities, initiatives, and utilization of the NASA Langley Research Center's Unitar...
Active 3-axis trim of a wind tunnel model in the Arnold Engineering Development Center’s (AEDC) Aero...
As part of a continuing effort to re-engineer the wind tunnel testing process, a comprehensive data ...
Ground-based infrastructure consisting of wind tunnels and propulsion system test cells has been the...
The evolution of remote controls used to position aerodynamic control surfaces on wind tunnel test a...
An overview of NASA Lewis' Aeropropulsion Wind Tunnel Productivity Improvements was presented at the...
For over half a century the NPS Aerolabʼ Low Speed Wind Tunnel located in Halligan Hall of the Nava...
The United States Air Force Precision Measurement Equipment Laboratories (PMEL) calibrate over 1,000...
Large aeronautical ground test facilities, particularly continuous flow wind tunnels and engine alti...
The 7 by 10 foot high speed tunnel performs a wide range of tests employing a variety of model insta...
This paper describes the results of two recent process improvements; drag feed-forward Mach number c...
The advantage of managing organizations to minimize product development cycle time has been well est...
After 4 years of existence, the Langley WTE is alive and growing. Significant improvements in the op...
Enhancing wind tunnel test productivity in terms of increased efficiency, reduced cost, and expanded...
Productivity gains have recently been made at the National Transonic Facility wind tunnel at NASA La...
Description, capabilities, initiatives, and utilization of the NASA Langley Research Center's Unitar...
Active 3-axis trim of a wind tunnel model in the Arnold Engineering Development Center’s (AEDC) Aero...
As part of a continuing effort to re-engineer the wind tunnel testing process, a comprehensive data ...
Ground-based infrastructure consisting of wind tunnels and propulsion system test cells has been the...
The evolution of remote controls used to position aerodynamic control surfaces on wind tunnel test a...
An overview of NASA Lewis' Aeropropulsion Wind Tunnel Productivity Improvements was presented at the...
For over half a century the NPS Aerolabʼ Low Speed Wind Tunnel located in Halligan Hall of the Nava...
The United States Air Force Precision Measurement Equipment Laboratories (PMEL) calibrate over 1,000...
Large aeronautical ground test facilities, particularly continuous flow wind tunnels and engine alti...
The 7 by 10 foot high speed tunnel performs a wide range of tests employing a variety of model insta...
This paper describes the results of two recent process improvements; drag feed-forward Mach number c...