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Aerodynamics of the Viggen 37 aircraft. Part 1: General characteristics at low speedA 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.
Document ID
19860019453
Document Type
Book
Authors
Karling, K. (NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1986
Subject Category
AERODYNAMICS
Report/Patent Number
NAS 1.15:88403
NASA-TM-88403
Funding Number(s)
CONTRACT_GRANT: NASW-4005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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