COMPARISON OF CALCULATED WITH MEASURED BOUNDARY-LAYER THICKNESSES ON THE CURVED WALLS OF THE JPL 20-IN. SUPERSONIC WIND TUNNEL TWODIMENSIONAL NOZZLE
Overview & Synopsis
Boundary layer thickness on curved walls of 20-in supersonic wind tunnel two-dimensional nozzle
Indexed from repository: NASA Technical Reports Server
(
ntrs.nasa.gov)
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Document Information
| Document Title | COMPARISON OF CALCULATED WITH MEASURED BOUNDARY-LAYER THICKNESSES ON THE CURVED WALLS OF THE JPL 20-IN. SUPERSONIC WIND TUNNEL TWODIMENSIONAL NOZZLE |
|---|---|
| Author / Organization | Dayman, B., Jr. |
| Subject & Discipline | CONTRACTOR_REPORT |
| Categories | Aerospace & Aviation |
| Publication Year | 2019 |
| License / Rights | Public Domain / NASA STI Open Access |
| Resource Verification | Listed PDF (Verification Pending) |
| Original Host Website |
NASA Technical Reports Server
(ntrs.nasa.gov)
|
| File Format | application/pdf (Portable Document Format) |
| Language | EN |
| Catalog ID | DOC-73062 |
| Original Source Link | Visit Source Page on ntrs.nasa.gov » |