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| Author | : Warren E. Anderson |
| Publisher | : |
| Total Pages | : 29 |
| Release | : 1952 |
| Genre | : |
| ISBN | : |
| Author | : L. Stewart Rolls |
| Publisher | : |
| Total Pages | : 22 |
| Release | : 1950 |
| Genre | : Aeronautics |
| ISBN | : |
The pressure-recovery characteristics at the vertical center line of an NACA submerged inlet of aspect ratio 5 have been measured in the Mach number range 0.60 to 1.08 by the wing-flow method. The variation of ram-recovery ratio determined from measurements at the center line of the inlet with test station Mach number is presented for mass-flow ratios of 0.30 to 0.60.
| Author | : Richard J. Re |
| Publisher | : |
| Total Pages | : 116 |
| Release | : 1976 |
| Genre | : Aerofoils |
| ISBN | : |
| Author | : Richard J. Re |
| Publisher | : |
| Total Pages | : |
| Release | : 1974 |
| Genre | : |
| ISBN | : |
| Author | : Charles F. Hall |
| Publisher | : |
| Total Pages | : 44 |
| Release | : 1948 |
| Genre | : Air ducts |
| ISBN | : |
The data indicate only a slight decrease in ram-recovery ratio for the inlets ahead of or just behind the wing leading edge as Mach number increased, but showed large decreases at high Mach numbers for the inlets aft of the point of maximum thickness of the wing.
| Author | : Richard Scherrer |
| Publisher | : |
| Total Pages | : 25 |
| Release | : 1955 |
| Genre | : |
| ISBN | : |
| Author | : Leonard J. Obery |
| Publisher | : |
| Total Pages | : 34 |
| Release | : 1953 |
| Genre | : |
| ISBN | : |
| Author | : Richard Scherrer |
| Publisher | : |
| Total Pages | : 37 |
| Release | : 1958 |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1954 |
| Genre | : |
| ISBN | : |
| Author | : Richard Scherrer |
| Publisher | : |
| Total Pages | : 22 |
| Release | : 1953 |
| Genre | : |
| ISBN | : |
