Discover Cryogenic Wind Tunnels

Microcomputer based controller for the Langley 0.3-meter Transonic Cryogenic Tunnel

A hybrid electronically scanned pressure module for cryogenic environments

A description of the active and passive sidewall-boundary-layer removal systems of the 0.3-Meter Transonic Cryogenic Tunnel

Development of a multi-component internal strain-gauge balance for model tests in a cryogenic wind tunnel

A study of a neon cycle cryogenic pumping system for a low density plasma tunnel

Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel

Hot-jet simulation in cryogenic wind tunnels

A simplified fourwall interference assessment procedure for airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel

A study of neon cycle cryogenic pumping system for a low density plasma tunnel

Computer program for calculating flow parameters and power requirements for cryogenic wind tunnels

Materials and techniques for model construction

Cryogenic wind tunnels

Acoustic properties and durability of liner materials at non-standard atmospheric conditions

Thermal sensing of cryogenic wind tunnel model surfaces

R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel

Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-Meter Transonic Cryogenic Tunnel

The construction of airfoil pressure models by the bonded plate method

Materials for cryogenic wind tunnel testing

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

Optimalsteuerungen - ein systematisches Hilfsmittel zur rechnergestutzten Erforschung der dynamischen Moglichkeiten eines Tieftemperaturwindkanals

Technology for pressure-instrumented thin airfoil models

Special course on advances in cryogenic wind tunnel technology

Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel