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Theoretical investigation of submerged inlets at low speeds (Published on: 01-08-1951)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sacks, Alvin H. Spreiter, John |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1951 |
| File Size | 2080099 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19930083005 |
| Archival Resource Key | ark:/13960/t18k8604v |
| Language | English |
| Publisher Date | 1951-08-01 |
| Publisher Institution | Ames Research Center |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Naca 64a010 - Char & Moments Wind Tunnel Tests - Aal (10'x7', No 1) Boundary Layer Control - Airfoils - Naca 64a010 Stalling - Wings Pressure Distribution - Airfoils - Naca 64a010 Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |