Author: D. G. Mabey
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Further Buffeting Tests in a Cryogenic Wind Tunnel
Further Buffeting Tests in a Cryogenic Wind Tunnel
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722411008
Category :
Languages : en
Pages : 62
Book Description
Further measurements of buffeting, using wing-root strain gauges, were made in the NASA Langley 0.3 m Cryogenic Wind Tunnel to refine techniques which will be used in larger cryogenic facilities such as the United States National Transonic Facility (NTF) and European Transonic Wind Tunnel (ETW). The questions addressed included the relative importance of variations in frequency parameter and Reynolds number, the choice of model material (considering both stiffness and damping) and the effects of static aeroelastic distortion. The main series of tests was made on half models of slender 65 deg delta wings with a sharp leading edge. The three delta wings had the same planform but widely different bending stiffness and frequencies (obtained by varying both the material and the thickness of the wings). It was known that the flow on this configuration would be insensitive to variations in Reynold number. Additional tests were made on one unswept half-wing of aspect ratio 1.5 with an NPL 9510 aerofoil section, known to be sensitive to variations in Reynolds number at transonic speeds. For brevity the test Mach numbers were restricted to M = 0.21 and 0.35 for the delta wings and to M = 0.30 for the unswept wing. Mabey, D. G. and Boyden, R. P. and Johnson, W. G., Jr. Langley Research Center...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722411008
Category :
Languages : en
Pages : 62
Book Description
Further measurements of buffeting, using wing-root strain gauges, were made in the NASA Langley 0.3 m Cryogenic Wind Tunnel to refine techniques which will be used in larger cryogenic facilities such as the United States National Transonic Facility (NTF) and European Transonic Wind Tunnel (ETW). The questions addressed included the relative importance of variations in frequency parameter and Reynolds number, the choice of model material (considering both stiffness and damping) and the effects of static aeroelastic distortion. The main series of tests was made on half models of slender 65 deg delta wings with a sharp leading edge. The three delta wings had the same planform but widely different bending stiffness and frequencies (obtained by varying both the material and the thickness of the wings). It was known that the flow on this configuration would be insensitive to variations in Reynold number. Additional tests were made on one unswept half-wing of aspect ratio 1.5 with an NPL 9510 aerofoil section, known to be sensitive to variations in Reynolds number at transonic speeds. For brevity the test Mach numbers were restricted to M = 0.21 and 0.35 for the delta wings and to M = 0.30 for the unswept wing. Mabey, D. G. and Boyden, R. P. and Johnson, W. G., Jr. Langley Research Center...
Cryogenic Wind Tunnels: A Comprehensive, Annotated Bibliography
Author: Marie H. Tuttle
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 146
Book Description
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 146
Book Description
Scientific and Technical Aerospace Reports
Structural Damping Studies at Cryogenic Temperatures
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
NASA Technical Memorandum
Monthly Catalog of United States Government Publications
The Shock and Vibration Digest
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1038
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1038
Book Description