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Vtol and vstol handling qualities specifications, an overview of the current status
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Goldstein, K. W. |
| Copyright Year | 1982 |
| Description | The highlights of a comparative analysis between the current helicopter and VSTOL specifications and four representative rotary wing aircraft are presented. Longitudinal, lateral, and directional control power and dynamic stability characteristics were analyzed for hovering conditions. Forward flight static and dynamic stability were analyzed for the longitudinal and lateral-directional axes. Results of the analyses in terms of the applicability/utility of the MIL-H-8501A criteria are presented for each of the above areas. The review of the MIL-H-8301A criteria against those in MIL-F-83300 and AGARD 577 indicate many areas in which MIL-H-8501A does not give adequate design guidance. |
| File Size | 549992 |
| Page Count | 7 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820015335 |
| Archival Resource Key | ark:/13960/t1jh8cp2q |
| Language | English |
| Publisher Date | 1982-04-01 |
| Access Restriction | Open |
| Subject Keyword | Air Transportation And Safety Military Helicopters Attitude Control V/stol Aircraft Longitudinal Control Helicopter Control Aircraft Specifications Controllability Control Stability Angle of Attack Flight Control Lateral Control Hovering Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
