NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Engineering and fabrication cost considerations for cryogenic wind tunnel modelsDesign and fabrication cost drivers for cryogenic transonic wind tunnel models are defined. The major cost factors for wind tunnel models are model complexity, tolerances, surface finishes, materials, material validation, and model inspection. The cryogenic temperatures require the use of materials with relatively high fracture toughness but at the same time high strength. Some of these materials are very difficult to machine, requiring extensive machine hours which can add significantly to the manufacturing costs. Some additional engineering costs are incurred to certify the materials through mechanical tests and nondestructive evaluation techniques, which are not normally required with conventional models. When instrumentation such as accelerometers and electronically scanned pressure modules is required, temperature control of these devices needs to be incorporated into the design, which requires added effort. Additional thermal analyses and subsystem tests may be necessary, which also adds to the design costs. The largest driver to the design costs is potentially the additional static and dynamic analyses required to insure structural integrity of the model and support system.
Document ID
19830010487
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Boykin, R. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Davenport, J. B., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1983
Publication Information
Publication: Cryogenic Wind Tunnel Models
Subject Category
Research And Support Facilities (Air)
Accession Number
83N18758
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available