Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Design Study of Test Models of Maneuvering Aircraft Configurations for the National Transonic Facility (NTF)
Design of Advanced Technology Maneuvering Aircraft Models for the National Transonic Facility
Author: S. A. Griffin
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
Book Description
The need for a large High-Reynolds-Number Transonic Wind Tunnel has long been recognized throughout the industry, both in the USA and Europe. Such a facility will provide a much needed tool for studying phenomena sensitive to Reynolds number. The National Transonic Facility (NTF), located at NASA Langley Research Center, is now in the calibration phase and has the desired capability. Its usefulness, however, will be greatly influenced by the ability of industry to develop model systems capable of withstanding the severe operating environment of the facility so necessary to achieve full-scale Reynolds number, without degradation of accuracy, and at reasonable cost. The basic objective of this engineering study was to determine the feasibility of designing models of advanced aerodynamic technology does offer the potential for making tunnel-to-full-scale data correlations for this type of aircraft configuration.
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
Book Description
The need for a large High-Reynolds-Number Transonic Wind Tunnel has long been recognized throughout the industry, both in the USA and Europe. Such a facility will provide a much needed tool for studying phenomena sensitive to Reynolds number. The National Transonic Facility (NTF), located at NASA Langley Research Center, is now in the calibration phase and has the desired capability. Its usefulness, however, will be greatly influenced by the ability of industry to develop model systems capable of withstanding the severe operating environment of the facility so necessary to achieve full-scale Reynolds number, without degradation of accuracy, and at reasonable cost. The basic objective of this engineering study was to determine the feasibility of designing models of advanced aerodynamic technology does offer the potential for making tunnel-to-full-scale data correlations for this type of aircraft configuration.
Design Study of Test Models of Maneuvering Aircraft Configurations for the National Transonic Facility
Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1984
Scientific and Technical Aerospace Reports
NASA SP.
Special Course on Advances in Cryogenic Wind Tunnel Technology
NASA Technical Memorandum
Cryogenic Wind Tunnels
Author: Marie H. Tuttle
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 116
Book Description
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 116
Book Description