Aspects of the design and construction of the Laminar Flow Supersonic Wind Tunnel at the NASA-Ames Fluid Mechanics Laboratory are discussed. The wind tunnel is to be used as part of the NASA High Speed Research Program (HSRP)
As the propulsion and power generation center of NASA, Lewis has designed its wind tunnels for propu...
A compilation of lectures presented at various Universities over a span of several years is discusse...
The goal of this project was to design and construct a small-scale, supersonic wind tunnel. The win...
The main objectives of this work is to demonstrate the potential of a cryogenic adaptive nozzle to g...
Low-disturbance or 'quiet' wind tunnels are now considered an essential part of meaningful boundary ...
This grant supported research into quiet-flow supersonic wind-tunnels, between May 1990 and December...
This grant supported research into quiet-flow supersonic wind-tunnels, between February 1994 and Feb...
This paper describes the requirements, design, and prototype testing of the flex-section and hinge s...
A unique, low-disturbance (quiet) supersonic wind tunnel has been commissioned at the NASA-Ames Flui...
This bibliography, with abstracts, consists of 298 citations arranged in chronological order. The ci...
Since Ludwieg tubes have been around for many years, and NASA has already established the feasibilit...
Laminar-turbulent transition in high speed boundary layers is a complicated problem which is still p...
The Boeing/AFOSR Mach-6 Quiet Tunnel has been achieving low-disturbance flow at high Reynolds number...
One of the principal design requirements for a quiet supersonic or hypersonic wind tunnel is to main...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
As the propulsion and power generation center of NASA, Lewis has designed its wind tunnels for propu...
A compilation of lectures presented at various Universities over a span of several years is discusse...
The goal of this project was to design and construct a small-scale, supersonic wind tunnel. The win...
The main objectives of this work is to demonstrate the potential of a cryogenic adaptive nozzle to g...
Low-disturbance or 'quiet' wind tunnels are now considered an essential part of meaningful boundary ...
This grant supported research into quiet-flow supersonic wind-tunnels, between May 1990 and December...
This grant supported research into quiet-flow supersonic wind-tunnels, between February 1994 and Feb...
This paper describes the requirements, design, and prototype testing of the flex-section and hinge s...
A unique, low-disturbance (quiet) supersonic wind tunnel has been commissioned at the NASA-Ames Flui...
This bibliography, with abstracts, consists of 298 citations arranged in chronological order. The ci...
Since Ludwieg tubes have been around for many years, and NASA has already established the feasibilit...
Laminar-turbulent transition in high speed boundary layers is a complicated problem which is still p...
The Boeing/AFOSR Mach-6 Quiet Tunnel has been achieving low-disturbance flow at high Reynolds number...
One of the principal design requirements for a quiet supersonic or hypersonic wind tunnel is to main...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
As the propulsion and power generation center of NASA, Lewis has designed its wind tunnels for propu...
A compilation of lectures presented at various Universities over a span of several years is discusse...
The goal of this project was to design and construct a small-scale, supersonic wind tunnel. The win...
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