Textual Modalities for: Wind tunnels
Records: Showing 20 of 976 total records
Page: 33 of 49
| Code | Title | Description | Source | Word Counts | URL |
|---|---|---|---|---|---|
| 344310.1 | Initial Whirl-Flutter Characterization of the TiltRotor Aeroelastic ...PDF | Therefore, a second wind tunnel test is planned that will ex-plore more configurations and fix some ... | Total words: 9,138 | wind: 21 | View | |
| 344310.1 | Our Legacy - NASA | 20-In Supersonic Wind Tunnel. Supersonic Flows. LANGLEY. Unitary Plan Wind Tunnels. 11-Ft Transonic ... | Total words: 438 | wind: 10 | tunnels: 5 | View | |
| 344310.1 | Aero-Thermal Calibration of the NASA Glenn Icing Research Tunnel | Research Tunnel (2012 Test) A major modification of the refrigeration plant and heat exchanger at th... | Total words: 977 | wind: 3 | tunnels: 2 | View | |
| 344310.1 | Altitude Wind Tunnel | Glenn Research Center | NASA | The Altitude Wind Tunnel (AWT), the nation’s first wind tunnel capable of studying full-scale engi... | Total words: 621 | wind: 10 | tunnels: 2 | View | |
| 344310.1 | Overview of the High Reynolds Number Ascent Wind Tunnel Test of the ... | •Previous SLS ascent wind tunnel tests were conducted at low Re D –Limited to 5x106(1-2 orders o... | Total words: 1,907 | wind: 8 | View | |
| 344310.1 | Supersonic Wind Tunnel Tests of a Half-axisymmetric 12 Deg-spike Inlet ... | Supersonic Wind Tunnel Tests of a Half-axisymmetric 12 Deg-spike Inlet to a Rocket-based Combined-cy... | Total words: 433 | wind: 3 | View | |
| 344310.1 | Post-stall wind tunnel data for NACA 44XX series airfoil sections | The purpose of this wind tunnel study is to characterize the performance characteristics of a blade ... | Total words: 704 | wind: 24 | tunnels: 2 | View | |
| 344310.1 | NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS - NASA Technical Reports ...PDF | Wind tunnel.- The wind tunnel, in the open jet of which these tests were conducted, is of convention... | Total words: 7,321 | wind: 4 | View | |
| 344310.1 | NTRS - NASA Technical Reports Server | Determinations of boundary-layer transition on the NACA 0012 and 2301 airfoils were made in the 8-fo... | Total words: 368 | wind: 5 | tunnels: 1 | View | |
| 344310.1 | Wind Tunnel Testing Perseverance’s Parachute - Science@NASA | In this June 2017 photo, the supersonic parachute design that will land NASA's Perseverance rover on... | Total words: 882 | wind: 3 | View | |
| 344310.1 | 20 Inch Supersonic Wind Tunnel (SWT) | Research Directorate - NASA | The 20-Inch Supersonic Wind Tunnel (SWT) is a versatile blow-down facility capable of producing supe... | Total words: 324 | wind: 4 | tunnels: 1 | View | |
| 344310.1 | Low Speed PSP Testing in Production Wind Tunnels | Low Speed PSP Testing in Production Wind Tunnels The brightness signal from a pressure-sensitive pai... | Total words: 281 | wind: 3 | tunnels: 3 | View | |
| 344310.1 | Wind-tunnel/flight correlation study of aerodynamic characteristics of ... | The results of calculations necessary to extrapolate performance data on an XB-70-1 wind tunnel mode... | Total words: 320 | wind: 4 | View | |
| 344310.1 | Design optimization and wind tunnel investigation of a flapping system ... | The critical parameters for the aerodynamic characteristics were investigated and optimized by means... | Total words: 1,017 | wind: 4 | View | |
| 344310.1 | NTRS - NASA Technical Reports Server | The NASA Glenn Research Center is currently participating in an American Institute of Aeronautics an... | Total words: 295 | wind: 2 | View | |
| 344310.1 | The NACA Tames its New Wind Tunnel - NASA | They explored a range of mitigation devices on a subscale model of the tunnel. The basic design for ... | Total words: 1,489 | wind: 9 | tunnels: 2 | View | |
| 344310.1 | Experimental and Computational Study of the X-59 Wind Tunnel Model at ... | Experimental and Computational Study of the X-59 Wind Tunnel Model at Glenn Research Center 8- by 6-... | Total words: 329 | wind: 6 | View | |
| 344310.1 | Historic Wind Tunnel Facility Testing NASA’s Mars Ascent Vehicle Rocket | By Jessica Barnett. The MAV (Mars Ascent Vehicle) team recently completed wind tunnel testing at NAS... | Total words: 1,555 | wind: 9 | tunnels: 1 | View | |
| 344310.1 | Loads Correlation of a Full-Scale UH-60A Airloads Rotor in a Wind TunnelPDF | A full-scale wind tunnel test of a UH-60A rotor was recently conducted (May 2010) by NASA and the U.... | Total words: 6,474 | wind: 14 | View | |
| 344310.1 | National Transonic Facility (NTF) | Research Directorate - NASA | The world’s largest pressurized cryogenic wind tunnel, th e National Transonic Facility (NTF), pos... | Total words: 177 | wind: 2 | View |
Page 33 of 49 (976 records)