Investigation Of Convergent Divergent Nozzles Applicable To Reduced Power Supersonic Cruise Aircraft
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Investigation of Installation Effects on Single-engine Convergent-divergent Nozzles
| Author | : James R. Burley |
| Publisher | : |
| Total Pages | : 244 |
| Release | : 1982 |
| Genre | : Aerodynamics |
| ISBN | : |
NASA Technical Paper
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 88 |
| Release | : 1992 |
| Genre | : Aeronautics |
| ISBN | : |
Static Performance of a Fixed-Geometry Exhaust Nozzle Incorporating Porous Cavities for Shock-Boundary Layer Interaction Control
| Author | : Scott C. Asbury |
| Publisher | : |
| Total Pages | : 142 |
| Release | : 1999 |
| Genre | : Boundary layer |
| ISBN | : |
