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Assessment of aerodynamic performance of v/stol and stovl fighter aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nelms, W. P. |
| Copyright Year | 1984 |
| Description | The aerodynamic performance of V/STOL and STOVL fighter/attack aircraft was assessed. Aerodynamic and propulsion/airframe integration activities are described and small and large scale research programs are considered. Uncertainties affecting aerodynamic performance that are associated with special configuration features resulting from the V/STOL requirement are addressed. Example uncertainties relate to minimum drag, wave drag, high angle of attack characteristics, and power induced effects. |
| File Size | 5129564 |
| Page Count | 38 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840014468 |
| Archival Resource Key | ark:/13960/t4wh7dm2s |
| Language | English |
| Publisher Date | 1984-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Evaluation V/stol Aircraft Ejectors Inlet Flow Aerodynamic Characteristics Fighter Aircraft Propulsion System Configurations Thrust Vertical Takeoff Aircraft Vector Currents Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
