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Computational analysis of hypersonic airbreathing aircraft flow fields
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Dwoyer, Douglas L. Kumar, Ajay |
| Copyright Year | 1987 |
| Description | The general problem of calculating the flow fields associated with hypersonic airbreathing aircraft is presented. Unique aspects of hypersonic aircraft aerodynamics are introduced and their demands on computational fluid dynamics are outlined. Example calculations associated with inlet/forebody integration and hypersonic nozzle design are presented to illustrate the nature of the problems considered. |
| File Size | 1136639 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870016586 |
| Archival Resource Key | ark:/13960/t11p30590 |
| Language | English |
| Publisher Date | 1987-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Navier-stokes Equation Computational Fluid Dynamics Supersonic Combustion Ramjet Engines Engine Airframe Integration Hypersonic Flow Air Breathing Engines Hypersonic Nozzles Hypersonic Aircraft Hypersonic Inlets Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
