Textual Modalities for: Wind tunnels
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Records: Showing 20 of 976 total records
Page: 44 of 49
| Code | Title | Description | Source | Word Counts | URL |
|---|---|---|---|---|---|
| 344310.1 | Transonic Dynamics Tunnel - NASAPDF | Tunnel NASA’s Aeronautics Test Program The Transonic Dynamics Tunnel (TDT) is a closed-circuit, co... | USA | Total words: 364 | wind: 2 | View |
| 344310.1 | Wind-tunnel investigation at supersonic speeds of a canard-controlled ...PDF | A wind tunnel investigation was made at free stream Mach numbers from 1.70 to 2.86 to determine the ... | USA | Total words: 255 | wind: 1 | View |
| 344310.1 | Our Legacy - NASA | 20-In Supersonic Wind Tunnel. Supersonic Flows. LANGLEY. Unitary Plan Wind Tunnels. 11-Ft Transonic ... | USA | Total words: 438 | wind: 10 | tunnels: 5 | View |
| 344310.1 | High-resolution flexible iontronic skins for both negative and positive ... | Flexible skins that can be laminated on curved surfaces are a desired form for wind pressure measure... | USA | Total words: 1,781 | wind: 12 | tunnels: 1 | View |
| 344310.1 | Aerodynamic noise in supersonic wind tunnels - NASA Technical Reports ... | Laufer, J. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States) | USA | Total words: 114 | wind: 2 | tunnels: 2 | View |
| 344310.1 | Use of the Ames Check Standard Model for the Validation of Wall ...PDF | The NASA Ames 11{ft Transonic Wind Tunnel uses a modi ed version of the wall signature method to est... | USA | Total words: 5,294 | wind: 48 | tunnels: 19 | View |
| 344310.1 | Ames 11-ft Wind Tunnel | NASA Common Research Model | The 11- by 11-Foot Transonic Wind Tunnel (11-Foot TWT) Facility is part of the Unitary Plan Wind Tun... | USA | Total words: 252 | wind: 3 | View |
| 344310.1 | The application of cryogenics to high Reynolds number testing in wind ... | The development and application of the cryogenic wind tunnel concept at the Langley Research Center ... | USA | Total words: 256 | wind: 5 | tunnels: 2 | View |
| 344310.1 | UH-60A Airloads Wind Tunnel Data Update - NASAPDF | Azimuthal Diff. Between Flight and Wind Tunnel" • Known 7 deg azimuth ref. difference between wind... | USA | Total words: 928 | wind: 18 | View |
| 344310.1 | 8- by 6-Foot Supersonic Wind Tunnel Description - NASA | Actively involved in research testing for over 60 years, the 8 X 6 is NASA’s only transonic-propul... | USA | Total words: 1,296 | wind: 6 | View |
| 344310.1 | NASA Common Research Model | providing data worldwidePDF | NASA Common Research Model | providing data worldwide | USA | Total words: 5,634 | wind: 57 | View |
| 344310.1 | Background noise in measuring section of low-noise acoustic wind ... | Even in low-noise wind tunnel where noise from the air-source fans has been almost entirely eliminat... | USA | Total words: 846 | wind: 16 | tunnels: 10 | View |
| 344310.1 | Application Of Artificial Intelligence To Wind Tunnels | Report discusses potential use of artificial-intelligence systems to manage wind-tunnel test facilit... | USA | Total words: 240 | wind: 2 | tunnels: 3 | View |
| 344310.1 | Protect Your Property from SEVERE WINDS - FEMA.govPDF | Protect Your Property from SEVERE WINDS - FEMA.gov | USA | Total words: 1,017 | wind: 11 | View |
| 344310.1 | Wind Tunnel Study of the Electro-Thermal De-Icing of Wind Turbine ... | @misc{etde_21108730, title = {Wind Tunnel Study of the Electro-Thermal De-Icing of Wind Turbine Blad... | USA | Total words: 706 | wind: 29 | tunnels: 1 | View |
| 344310.1 | Noise measurement in wind tunnels, workshop summary | In reviewing the progress made in acoustic measurements in wind tunnels over the 5-yr span of the wo... | USA | Total words: 288 | wind: 3 | tunnels: 3 | View |
| 344310.1 | High Lift Prediction Workshop 5 - Wind Tunnel Data - NASA | The wind tunnel data are not all being released at once. Some are being held back purposefully, so t... | USA | Total words: 285 | wind: 3 | View |
| 344310.1 | Abe Silverstein Supersonic Wind Tunnel (SWT) (10x10) Quick Facts - NASA | The Abe Silverstein Supersonic Wind Tunnel (10×10) was designed to test supersonic propulsion compo... | USA | Total words: 1,131 | wind: 7 | View |
| 344310.1 | NASA Technical Reports Server (NTRS)PDF | %PDF-1.4 %âãÏÓ 726 0 obj /Linearized 1 /O 728 /H [ 1073 449 ] /L 3670444 /E 15353 /N 104 /T 3655... | USA | Total words: 6,360 | wind: 1 | View |
| 344310.1 | NTRS - NASA Technical Reports Server | Numerical solutions of the differential equation obtained from the momentum theorem for the developm... | USA | Total words: 365 | wind: 2 | View |
Page 44 of 49 (976 records)