Aerodynamics of the Viggen 37 aircraft. Part 1 : General characteristics at low speed
- Karling, K.
- Jun 1, 1986.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available. and Free-to-read Unrestricted online access
- A description of the aerodynamics of the Viggen 37 and its performances, especially at low speeds is presented. The aerodynamic requirements for the design of the Viggen 37 aircraft are given, including the basic design, performance requirement, and aerodynamic characteristics, static and dynamic load test results and flight test results. The Viggen 37 aircraft is designed to be used for air attack, surveillance, pursuit, and training applications. It is shown that this aircraft is suitable for short runways, and has good maneuvering, acceleration, and climbing characteristics. The design objectives for this aircraft were met by utilizing the effect produced by the interference between two triangular wings, positioned in tandem.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19860019453., Accession ID: 86N28925., NASA-TM-88403., and NAS 1.15:88403.
- No Copyright.
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