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Force and moment data from a wind-tunnel test of a tilt-nacelle v/stol propulsion system with an attitude control vane. [conducted in ames 40 by 80 foot wind tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Betzina, M. D. |
| Copyright Year | 1979 |
| Description | A large scale, tilt nacelle V/STOL propulsion system, with an attitude control vane assembly mounted in the exhaust, was tested. The effectiveness of the control vane as well as the aerodynamic characteristics of the entire propulsion system were determined. The results, in the form of tabulated coefficients, for both the vane forces and moments and the total forces and moments produced by the propulsion system are presented. |
| File Size | 3332616 |
| Page Count | 107 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800004748 |
| Archival Resource Key | ark:/13960/t2s51g82x |
| Language | English |
| Publisher Date | 1979-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics V/stol Aircraft Propulsion System Performance Systems Engineering Control Surfaces Wind Tunnel Tests Nacelles Aerodynamic Forces Aerodynamic Characteristics Stability Derivatives Exhaust Systems Guide Vanes Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |