Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19650033496

The hyperthermal supersonic aerodynamic tunnel.

View original source ↗Export metadata ↓

Abstract

Electric-arc-heated hyperthermal wind tunnel operation and improvement by enthalpy output increase and optimal use at tunnel throat

Explore related subjects

WIND TUNNEL ARC HEATING

Keep this discovery

Explore connections, maps & timelines

Stine, H. A.. 1964-01-01. The hyperthermal supersonic aerodynamic tunnel.. https://ntrs.nasa.gov/citations/19650033496

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

NASA NTRS1967

Aerodynamics of free-flying wind-tunnel models determined from telemetered accelerations.

Total aerodynamic forces and moments of free flying body in wind tunnel determined from accelerations measured and telemetered by onboard instruments

WIND TUNNEL↗

NASA NTRS1967

Mixing devices for delaying separation

High speed wind tunnel study of separation phenomenon and deterioration in aerodynamic performance from unwanted flow detachments

WIND TUNNEL↗

NASA NTRS1966

Wind-tunnel investigation of thermal and pressure environments in the base of the Saturn S-IC booster from Mach 0.1 to 3.5

Wind tunnel testing of thermal and pressure in base of Saturn S-IC booster

WIND TUNNEL↗