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 |
Page 8 of 49 (976 records)