Textual Modalities for: Wind tunnels

Records: Showing 20 of 976 total records Page: 8 of 49
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344310.1 Design and Evaluation of a Pressure Rail for Sonic Boom Measurement in ...PDF Wind tunnel humidity and pressure variations over time and model lift changes due to translation thr... Total words: 8,496 | wind: 44 | tunnels: 3 View
344310.1 Surface flow visualization using indicators - NASA Technical Reports ... Surface flow visualization using indicators in the cryogenic wind tunnel which requires a fresh look... Total words: 258 | wind: 4 | tunnels: 3 View
344310.1 Computational Design and Analysis of a Transonic Natural Laminar Flow ...PDF II. Design of the Wind Tunnel Model The proposed wind tunnel test will focus on quantifying laminar ... Total words: 8,295 | wind: 52 | tunnels: 4 View
344310.1 Videogrammetric Model Deformation Measurement TechniquePDF deformation may be defined as the change in shape of a wind tunnel model (particularly the wings and... Total words: 7,936 | wind: 37 | tunnels: 14 View
344310.1 NASA Technical Memorandum 83197 - NASA Technical Reports Server (NTRS)PDF Flow Hypersonic Tunnel (CFHT) and in the Langley Hypersonic CF4 Tunnel (CF4 Tunnel). Thin-film gages... Total words: 15,953 | wind: 17 | tunnels: 18 View
344310.1 Wind-Tunnel to Full-Scale Mapping of Winds and Loads for Launch-Vehicle ...PDF map wind-tunnel acquired winds and loads to equivalent full-scale values applicable to modern launch... Total words: 9,414 | wind: 173 View
344310.1 Wall Correction Methods | NASA Common Research Model Both the NTF and the Ames 11-ft wind tunnels use the Transonic Wall Interference Correction System (... Total words: 609 | wind: 4 | tunnels: 2 View
344310.1 (1951) Portable Wind Tunnel and Dust Collector Developed to Evaluate ...PDF Portable Wind Tunnel Portable wind tunnels have been constructed pre- viously to study wind erosion ... Total words: 1,904 | wind: 22 | tunnels: 1 View
344310.1 Critical Assessment of Wind Tunnel Results for the NACA 0012 AirfoilPDF ORPGmm PAGk I,., A. Develowent of the Process OF POOR Q'FJALETY 1-3 The critical information used in... Total words: 8,253 | wind: 21 | tunnels: 11 View
344310.1 SLD Instrumentation in Icing Wind Tunnels – Investigation Overview The wind tunnel has two test sections available: 1) a 57 cm wide by 57 cm high test section, contrac... Total words: 7,309 | wind: 29 | tunnels: 9 View
344310.1 Reduction of turbulence in wind tunnels - NASA Technical Reports Server ... Reduction of turbulence in wind tunnels A brief nonmathematical outline is given of modern views as ... Total words: 233 | wind: 4 | tunnels: 3 View
344310.1 NASA Wind Tunnel “Bad Days”PDF accuracy and efficiency of CFD compared to wind tunnel testing for past, present, and future problem... Total words: 2,102 | wind: 26 | tunnels: 7 View
344310.1 Wind-Tunnel Model Systems Criteria - NASA Unitary Plan Wind Tunnel 8-Foot High Temperature Tunnel In addition, drop model systems and remotely... Total words: 16,983 | wind: 28 | tunnels: 4 View
344310.1 NASA Ames Balance Basics A wind tunnel balance is a device that measures the aerodynamic loads a model experience during a wi... Total words: 1,273 | wind: 6 View
344310.1 CFD and experimental data of closed-loop wind tunnel flow The data presented in this article were the basis for the study reported in the research articles en... Total words: 2,210 | wind: 60 | tunnels: 1 View
344310.1 Hypersonic Wind Tunnel - Research Justin Smith Sandia National Laboratories PO Box 5800, MS 0825 Albuquerque, NM 87185 jussmit@sandia.... Total words: 66 | wind: 4 | tunnels: 1 View
344310.1 TECHNICAL NASA TRPDF tunnel boundary is partly open and partly closed (e.g., slotted), the interference may pro­ duce ei... Total words: 3,859 | wind: 3 | tunnels: 2 View
344310.1 Flow Visualization to Complement Modern Wind Tunnel TestingPDF 1 Garbeff, Baerny, Ross, “Wind Tunnel Flow Field Visualizations of the Space Launch System Vehicle... Total words: 697 | wind: 9 View
344310.1 Enabling Advanced Wind Tunnel Research Methods Using the NASA Langley ...PDF 12-Foot Low Speed Tunnel. The GL-10 full-scale UAV design, the prototype flight vehicle, and the win... Total words: 9,714 | wind: 67 View
344310.1 Wind Tunnel Performance Tests of a Full-Scale Proprotor on the ... The first wind-tunnel entry was completed in November 2018 with a modern, 26-ft diameter proprotor. ... Total words: 312 | wind: 4 View
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