Textual Modalities for: Wind tunnels
Records: Showing 20 of 976 total records
Page: 37 of 49
| Code | Title | Description | Source | Word Counts | URL |
|---|---|---|---|---|---|
| 344310.1 | Wind Tunnel Testing a Full-Sized Aircraft Tail - NASA | NASA recently tested a full-sized tail from a 757 commercial aircraft that was modified and equipped... | Total words: 1,080 | wind: 4 | View | |
| 344310.1 | 9- by 15-Foot Low Speed Wind Tunnel Acoustic Improvements Expanded OverviewPDF | The 9- by 15-Foot Low Speed Wind Tunnel (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ... | Total words: 1,534 | wind: 8 | View | |
| 344310.1 | Wall and blockage effects on air speed calibrations | NIST | Typically, wind tunnels used for calibration generate low-turbulence, high-speed flows by straighten... | Total words: 467 | wind: 4 | tunnels: 2 | View | |
| 344310.1 | The Unitary Plan Wind Tunnels - NASA Technical Reports Server (NTRS)PDF | The Unitary Plan Facility is the most heavily used wind tunnel in all of NASA. Every major commercia... | Total words: 234 | wind: 4 | tunnels: 2 | View | |
| 344310.1 | Wind Tunnel - Activity - NASA | The wind tunnel test section (A), as in some operating wind tunnels, can be resized by moving the wa... | Total words: 497 | wind: 8 | tunnels: 1 | View | |
| 344310.1 | NTRS - NASA Technical Reports Server | This report presents the data acquired during the testing of an individual blade control (IBC) syste... | Total words: 780 | wind: 6 | View | |
| 344310.1 | AN OVERVIEW OF PRELIMINARY COMPUTATIONAL AND EXPERIMENTAL RESULTS FOR ...PDF | tant component of each wind-tunnel test. Typically, one GVT was performed prior to every wind-tunnel... | Total words: 5,860 | wind: 6 | View | |
| 344310.1 | Airloads Correlation of the UH-60A Rotor Inside the 40- by 80-Foot Wind ...PDF | airloads remain. One possible cause for these differences is the simplified CFD modeling of the wind... | Total words: 6,353 | wind: 87 | View | |
| 344310.1 | Wall interference in a two-dimensional-flow wind tunnel, with ... | Theoretical tunnel-wall corrections are derived for an airfoil of finite thickness and camber in a t... | Total words: 224 | wind: 3 | View | |
| 344310.1 | CFD Validation of High-Lift Flows with Significant Wind-Tunnel EffectsPDF | ulate wind-tunnel facilities in their CFD calculations. Muc h of the researc hin this area has fo cu... | Total words: 8,771 | wind: 17 | tunnels: 1 | View | |
| 344310.1 | An Assessment of Methods for Determining Wind Loads - NISTPDF | Boundary Layer Wind Tunnel Laboratory University of Western Ontario, London, ON, Canada N6A 589 Arin... | Total words: 4,711 | wind: 149 | tunnels: 2 | View | |
| 344310.1 | Advancing Test Capabilities at NASA Wind TunnelsPDF | • Greatly enhance optical access for instruments in 11x11 and 9x7 wind tunnels at ARC, by cutting ... | Total words: 1,755 | wind: 6 | tunnels: 4 | View | |
| 344310.1 | Characterization of Freestream Disturbances in Conventional Hypersonic ... | @conference{osti_1483114, author = {Duan, Lian and Choudhari, Meelan and Chou, Amanda and Munoz, Fed... | Total words: 390 | wind: 7 | tunnels: 7 | View | |
| 344310.1 | FULL-SCALE WIND TUNNEL TEST OF A UH-60 INDIVIDUAL BLADE CONTROL SYSTEM ...PDF | Rotor Test Apparatus in the NFAC 40-by 80-Foot Wind Tunnel. Previous wind tunnel experiments (Ref. 3... | Total words: 10,413 | wind: 35 | View | |
| 344310.1 | Advancing Test Capabilities at NASA Wind Tunnels | NASA maintains twelve major wind tunnels at three field centers capable of providing flows at 0.1 M ... | Total words: 464 | wind: 10 | tunnels: 8 | View | |
| 344310.1 | X-48B in Langley Wind Tunnel - NASA | Researchers at NASA's Langley Research Center in Hampton, VA, tested the a 21-foot wingspan 8.5 perc... | Total words: 986 | wind: 4 | View | |
| 344310.1 | Computational and Experimental Characterization of the Mach 6 Facility ...PDF | HE Arc-Heated Scramjet Test Facility (AHSTF)1–3 is a high-enthalpy wind tunnel used for testing su... | Total words: 9,561 | wind: 1 | View | |
| 344310.1 | Calibration of transonic and supersonic wind tunnels | State-of-the art instrumentation and procedures for calibrating transonic (0.6 less than M less than... | Total words: 327 | wind: 3 | tunnels: 7 | View | |
| 344310.1 | Wind Tunnel and Field Evaluation of Trapping Efficiency of ... | Wind tunnel experiments were performed in the University of Guelph Engineering Boundary Layer Wind T... | Total words: 7,789 | wind: 45 | tunnels: 2 | View | |
| 344310.1 | Experimental Aeroheating Study in NASA LaRC 20-Inch Mach 6 Air Tunnel ...PDF | Wind Tunnel Model . The BOLT Step Test (BST) model, which was developed for testing with an infrared... | Total words: 7,387 | wind: 40 | tunnels: 2 | View |
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