Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19640030196

Fluctuating wall pressure under a separated supersonic flow.

View original source ↗Export metadata ↓

Abstract

Fluctuating wall pressure under separated supersonic turbulent boundary layer, showing origins of fluctuations

Explore related subjects

SEPARATED FLOW PRESSURE OSCILLATION SUPERSONIC FLOW TURBULENT BOUNDARY LAYER WALL PRESSURE

Keep this discovery

Explore connections, maps & timelines

Kistler, A. L.. 1964-03-01. Fluctuating wall pressure under a separated supersonic flow.. https://ntrs.nasa.gov/citations/19640030196

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

KEEP EXPLORING

Related reports

NASA NTRS1966

An analytical study of separated flows induced by shock wave - Boundary layer interaction

Analytical study of separated flows induced by shock wave-boundary layer interaction

SEPARATED FLOW↗

NASA NTRS1966

Static and fluctuating pressures in regions of separated flow.

Wind tunnel analysis of separated flow in region of several two-dimensional flow perturbations, presenting fluctuating pressure levels as function of Mach number for undisturbed flow

SEPARATED FLOW↗

NASA NTRS1965

Performance of five ablation materials as coating for structures in a region of separated flow

Commercially available ablation materials for use as thermal protection for sidewalls of advanced air-to-air missiles - protective coatings for structures in separated flow region

SEPARATED FLOW↗