Textual Modalities for: Wind tunnels
Records: Showing 20 of 976 total records
Page: 14 of 49
| Code | Title | Description | Source | Word Counts | URL |
|---|---|---|---|---|---|
| 344310.1 | Wright Wind Tunnel Models - NASA | The wind tunnel tests were conducted from September to December of 1901. At the conclusion of the te... | Total words: 1,547 | wind: 5 | View | |
| 344310.1 | NATIONAL TRANSONIC FACILITY MODEL AND TUNNEL VIBRATIONSPDF | the airfoil in the tunnel to the lift in free air. Most of the discussion in the ensuing aeroelastic... | Total words: 4,798 | wind: 23 | tunnels: 6 | View | |
| 344310.1 | IFASD 2024: Experimental Investigation of a Highly Flexible Wing for ...PDF | Infrastructures, methodologies •Wind Tunnel 1, ZHAW, Winterthur, closed test section, •Wind Tunn... | Total words: 839 | wind: 23 | tunnels: 3 | View | |
| 344310.1 | Wind Tunnel Force Balance Calibration Study – Interim ResultsPDF | Wind tunnel force balances utilized for testing in NASA programs include single and multi-piece desi... | Total words: 2,326 | wind: 8 | View | |
| 344310.1 | for Reducing Free-Stream Turbulence in Wind TunnelsPDF | wind tunnels have little, if any, settling chamber between the turning vanes and the start of the co... | Total words: 9,918 | wind: 35 | tunnels: 16 | View | |
| 344310.1 | TECHNICAL NOTEPDF | Part III- Wind Tunnels Having Width-Height Ratio of 1.O. NASA TND-935, 1962. 5. Heyson, Harry H.: Ta... | Total words: 35,390 | wind: 4 | tunnels: 7 | View | |
| 344310.1 | Drag Balance - Operation | Glenn Research Center | NASA | As the test begins, the tunnel is turned off and a model is placed on the cross beam of the balance.... | Total words: 1,009 | wind: 2 | View | |
| 344310.1 | The AEDC 10-Deg Cone Wind Tunnel/Flight Laminar-Turbulent Correlation ... | Its utility was extended to subsonic wind tunnels as well. The earlier cone produced the Pate and Sc... | Total words: 13,004 | wind: 129 | tunnels: 101 | View | |
| 344310.1 | Analysis of NASA Common Research Model Dynamic DataPDF | Facility (NTF) and Ames 11-foot Transonic Wind Tunnel (11-foot TWT) have generated an experimental d... | Total words: 5,276 | wind: 11 | tunnels: 1 | View | |
| 344310.1 | Ames Wind Tunnel - NASA | Construction of the Ames wind tunnel and its original 40- by 80-foot test section. A later expansion... | Total words: 898 | wind: 3 | View | |
| 344310.1 | NASA Center Boosted YF-12 Supersonic Engine Research | Lewis’ researchers had studied supersonic inlets in wind tunnels since the early 1950s and were in... | Total words: 1,672 | wind: 6 | tunnels: 3 | View | |
| 344310.1 | History of Wind Tunnels - grc.nasa.gov | In a wind tunnel, the axial centerline of the test section defines the direction of the oncoming win... | Total words: 3,213 | wind: 28 | tunnels: 6 | 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... | Total words: 20,483 | wind: 225 | tunnels: 19 | 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... | Total words: 20,483 | wind: 225 | tunnels: 19 | View | |
| 344310.1 | Description and Calibration of the Langley Unitary | WIND TUNNEL AND EQUIPMENT Wind Tunnel Arrangement.- The Langley Unitary Plan Wind Tunnel is a closed... | Total words: 10,726 | wind: 37 | tunnels: 1 | View | |
| 344310.1 | Wind Tunnel Test Technique and Instrumentation Development at LaRCPDF | Wind Tunnel Test Technique and Instrumentation Development at LaRC N By Lawrence E. Pumam Presented ... | Total words: 1,168 | wind: 1 | View | |
| 344310.1 | Wind Tunnel Balance Calibration: Are 1,000,000 Data Points Enough? | Wind tunnel balances are one such measurement system. Many different calibration systems, load sched... | Total words: 487 | wind: 5 | 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... | Total words: 20,483 | wind: 225 | tunnels: 19 | View | |
| 344310.1 | Experimental Study of Fillets to Reduce Corner Effects in an Oblique ...PDF | layer toward the floor of the wind tunnel and into the corner region. Because of the subsonic layer ... | Total words: 8,102 | wind: 11 | tunnels: 1 | View | |
| 344310.1 | NASA TECHNICAL NOTE 6827PDF | AY E uncertainty in the measurement of specific-heat ratio recovery factor DESCMPTION OF' APPARATUS ... | Total words: 8,033 | wind: 11 | tunnels: 2 | View |
Page 14 of 49 (976 records)