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Design Of High Reynolds Number Flat Plate Experiments In The Ntf by W. S. Saric
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1NASA Technical Reports Server (NTRS) 19890004040: Design Of High-Reynolds-number Flat-plate Experiments In The NTF
By NASA Technical Reports Server (NTRS)
The design of an experiment to measure skin friction and turbulent boundary layer characteristics at Reynolds numbers exceeding 1 x 10 to the 9th is described. The experiment will be conducted in a zero-pressure-gradient flow on a flat plate in the National Transonic Facility (NTF). The development of computational codes to analyze the aerodynamic loads and the blockage is documented. Novel instrumentation techniques and models, designed to operate in cryogenic environments, are presented. Special problems associated with aerodynamic loads, surface finish, and hot-wire anemometers are discussed.
“NASA Technical Reports Server (NTRS) 19890004040: Design Of High-Reynolds-number Flat-plate Experiments In The NTF” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19890004040: Design Of High-Reynolds-number Flat-plate Experiments In The NTF
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19890004040: Design Of High-Reynolds-number Flat-plate Experiments In The NTF” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - DESIGN ANALYSIS - FLAT PLATES - HIGH REYNOLDS NUMBER - TRANSONIC WIND TUNNELS - AERODYNAMIC LOADS - BOUNDARY LAYER FLOW - CODING - COMPUTATIONAL FLUID DYNAMICS - HOT-WIRE ANEMOMETERS - PRESSURE GRADIENTS - SKIN FRICTION - SURFACE FINISHING - TURBULENCE - Saric, William S.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19890004040
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