Textual Modalities for: Wind tunnels
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Records: Showing 20 of 976 total records
Page: 16 of 49
| Code | Title | Description | Source | Word Counts | URL |
|---|---|---|---|---|---|
| 344310.1 | Background-Oriented Schlieren for Large-Scale and High-Speed ...PDF | of the subsonic wind tunnel. The wind tunnel has an octagonal cross section with an inner diameter o... | USA | Total words: 3,883 | wind: 11 | View |
| 344310.1 | 1901 Wind Tunnel Tests | Glenn Research Center | NASA | The wind tunnel tests were conducted from September to December of 1901. At the conclusion of the te... | USA | Total words: 828 | wind: 9 | View |
| 344310.1 | Evaluation of flow quality in two large nasa wind tunnels at transonic ... | recognized, and work is being done to develop such tunnels (refs. 9 and 10). Based on very limited i... | USA | Total words: 13,600 | wind: 42 | tunnels: 65 | View |
| 344310.1 | NASA Ames Research Center Archives | The World's Largest Wind Tunnels: Their History, Contributions to Aeronautics, and Importance to Fli... | USA | Total words: 1,163 | wind: 2 | tunnels: 2 | View |
| 344310.1 | HIGH TUNNEL SYSTEM - Natural Resources Conservation ServicePDF | Where wind loads may damage the structure, select the tunnel cover and structure designed by the man... | USA | Total words: 1,583 | wind: 6 | tunnels: 3 | View |
| 344310.1 | Wind tunnel tests on a large astronomical telescope - FermilabPDF | 4. Calculation of predicted aerodynamic loads for the wind tunnel scale and conditions, using in par... | USA | Total words: 2,932 | wind: 52 | View |
| 344310.1 | V/STOL tilt rotor aircraft study: Wind tunnel tests of a full scale ... | The rotor system designed for the Boeing Model 222 tilt rotor aircraft is a soft-in-plane hingeless ... | USA | Total words: 268 | wind: 3 | View |
| 344310.1 | A New Method of Testing in Wind Tunnels - NASA Technical Reports Server ...PDF | Now, in existing wind tunnels, using a horsepower of 100 to 300, the models are generally made to a ... | USA | Total words: 290 | wind: 6 | tunnels: 4 | View |
| 344310.1 | A stereo photogrammetry system for model position and attitude ... | In this paper, a measurement system based on stereo photogrammetry is proposed for position and atti... | USA | Total words: 962 | wind: 11 | View |
| 344310.1 | Flow Visualization - NASA | Aerodynamicists use wind tunnels to test models of proposed aircraft and engine components. During a... | USA | Total words: 361 | wind: 7 | tunnels: 1 | View |
| 344310.1 | Wind pressure on a model of the Empire State Building - NISTPDF | 496 BureauofStandardsJournalofResearch [Vol.10 connectioncouldthenbemadethroughtheinteriorofthemodel... | USA | Total words: 4,187 | wind: 34 | tunnels: 1 | View |
| 344310.1 | Navier-Stokes, Flight, and Wind Tunnel Flow Analysis for the F/A-18 ...PDF | wind tunnel Reynolds numbcrs produces negligible effects on the forcbody and the LEX surface pres-su... | USA | Total words: 8,665 | wind: 11 | tunnels: 2 | View |
| 344310.1 | Inventor of Air Conditioning Helped Chill NASA Wind Tunnels | NACA engineers were experts in wind tunnel design, but simulating 30,000-foot altitudes to test full... | USA | Total words: 1,658 | wind: 11 | tunnels: 4 | View |
| 344310.1 | Test Planning Guide for High Speed Wind Tunnels A027-9391-XB2 TPG v8 - NASA | Wind Tunnel Division, National Aeronautics and Space Administration, Ames Research Center, Moffett F... | USA | Total words: 20,483 | wind: 225 | tunnels: 19 | View |
| 344310.1 | Unitary Plan Wind Tunnels Presentation (1955) - Glenn Research CenterPDF | UNITARY PLAN WIND TUNNELS presented by Unitary Plan Wind Tunnel Divisi on '. T. his wind tunnel is o... | USA | Total words: 2,629 | wind: 27 | tunnels: 5 | View |
| 344310.1 | X-59 Model Tested in Wind Tunnel in Japan - NASA | The scale model of the X-59 is suspended in the test area of JAXA’s wind tunnel as a researcher pr... | USA | Total words: 1,480 | wind: 12 | tunnels: 2 | View |
| 344310.1 | Investigation of air flow in open-throat wind tunnels | Tests were conducted on the 6-inch wind tunnel of the National Advisory Committee for Aeronautics to... | USA | Total words: 268 | wind: 5 | tunnels: 4 | View |
| 344310.1 | Reduction of Background Noise in the NASA Ames 40- by 80- Foot Wind TunnelPDF | Foot Wind Tunnel, the principle background noise sources can be classified as: 1) fan drive noise 2)... | USA | Total words: 327 | wind: 1 | View |
| 344310.1 | Within-Tunnel Variations in Pressure Data for Three Transonic Wind TunnelsPDF | model of wind tunnel testing that has evolved over time. By this model, data are regarded as the pro... | USA | Total words: 16,297 | wind: 35 | tunnels: 24 | View |
| 344310.1 | Comparison of the NASA Common Research Model European Transonic Wind ...PDF | The Ames Unitary Plan Wind Tunnel (UPWT) consists of three tunnel legs: the 11-by-11-Foot Transonic ... | USA | Total words: 6,274 | wind: 48 | tunnels: 9 | View |
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