Search NASA⌕ Search
Home/Archive/NASA NTRS

NASA NTRS · 19660061819

Bluntness and boundary-layer displacement effects on hypersonic inlet flowfields.

Benson, J. L.·Maslowe, S. A.
View original source ↗Export metadata ↓

Abstract

Bluntness and boundary layer displacement effects on air breathing engine hypersonic inlet flow fields

Explore related subjects

INLET FLOWBLUNT BODYFLOW FIELDHYPERSONIC BOUNDARY LAYERAIR BREATHING ENGINE

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Benson, J. L., Maslowe, S. A.. 1966-09-01. Bluntness and boundary-layer displacement effects on hypersonic inlet flowfields.. https://ntrs.nasa.gov/citations/19660061819

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

KEEP EXPLORING

Related reports

NASA NTRS1967

Experimental Evaluation of Transonic Stators Preliminary Analysis and Design Report

A flow-generating rotor has been designed under NASA contract NAS3-7614 to enable three transonic stators to be tested. The stators were designed by NASA in conjunction with the Contractor. Design analyses were conducted and the results indicate that the rotor will produce the required inlet flow to the stators. Structural and vibration analyses indicate that resonances and critical speeds occur outside the operating range and that the component stresses will be well within the capabilities of the materials used. Design details of the flow generation rotor and the three transonic stators are presented.

INLET FLOW↗