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An experimental and analytical investigation of the aerodynamics of a hypersonic vehicle at free stream mach 6
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Parikh, H. Zakkay, V. Munakata, A. Wang, C. R. |
| Copyright Year | 1981 |
| Description | The goal of this research is the assessment of the validity of existing three dimensional numerical programs in the prediction of the flow fields about general three dimensional hypersonic bodies. A detailed experimental research program was performed in which surface and flow field pressures were mapped. The results of the experimental work were compared with existing inviscid programs. Improvements were made on the existing numerical methods to include angle of attack. A summary of this work is presented. |
| File Size | 922977 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810012497 |
| Archival Resource Key | ark:/13960/t0bw2976c |
| Language | English |
| Publisher Date | 1981-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Hypersonics Three Dimensional Flow Flow Distribution Pressure Distribution Inviscid Flow Reentry Vehicles Angle of Attack Free Flow Hypersonic Vehicles Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
