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Aerodynamic characteristics and flying qualities of a tailless triangular-wing airplane configuration as obtained from flights of rocket-propelled models at transonic and supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1956 |
| Description | A flight investigation of rocket-powered models of a tailless triangular-wing airplane configuration was made through the transonic and low supersonic speed range at the Langley Pilotless Aircraft Research Station at Wallops Island, Va. An analysis of the aerodynamic coefficients, stability derivatives, and flying qualities based on the results obtained from the successful flight tests of three models is presented. |
| File Size | 26189859 |
| Page Count | 59 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930084649 |
| Archival Resource Key | ark:/13960/t6b32kt9g |
| Language | English |
| Publisher Date | 1956-11-01 |
| Access Restriction | Open |
| Subject Keyword | Damping Derivatives - Stability Stability, Longitudinal - Dynamic Airplanes - Specific Types Control, Longitudinal Control, Hinge Moments Wing-fuselage Combinations - Airplanes Mach Number Effects - Complete Wings Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |