Textual Modalities for: Wind tunnels
Source Filter: usa.gov Clear Filter
Records: Showing 20 of 976 total records
Page: 10 of 49
| Code | Title | Description | Source | Word Counts | URL |
|---|---|---|---|---|---|
| 344310.1 | A Preliminary Study of Inter-Facility LWC Differences in Appendix C and ...PDF | Wind tunnel facilities have adopted different instrumentation for liquid water content measurement, ... | USA | Total words: 6,279 | wind: 20 | tunnels: 9 | View |
| 344310.1 | Measuring Drag Coefficient in a Wind Tunnel - NASA | DESCRIPTION: A set of activities using a student wind tunnel. CONTRIBUTED BY: Carol Hodanbosi EDITED... | USA | Total words: 854 | wind: 12 | View |
| 344310.1 | TunnelSys - Application Downloads - NASA | The wind tunnel test program is used to obtain the lift of the wing model designed using the Design ... | USA | Total words: 1,255 | wind: 17 | tunnels: 2 | View |
| 344310.1 | Ames Wind Tunnel Historic District National Register of Historic ... - NASAPDF | portions of the wind tunnel on the west side. The interior of the building contains the controls for... | USA | Total words: 17,091 | wind: 315 | tunnels: 112 | View |
| 344310.1 | Ares I Aerodynamic Testing at the Boeing Polysonic Wind TunnelPDF | balances were used (typically 30lbs on axial force). The use of this wind tunnel for supersonic Mach... | USA | Total words: 4,500 | wind: 23 | View |
| 344310.1 | Laser Doppler Velocimetry - LDV - NASA | In some wind tunnel tests, the model is instrumented to provide diagnostic information about the flo... | USA | Total words: 530 | wind: 2 | tunnels: 1 | View |
| 344310.1 | WIND TUNNEL INTERFERENCE FACTORS FOR HIGH-LIFT WINGS IN CLOSED WIND TUNNELSPDF | WIND TUNNEL INTERFERENCE FACTORS FOR HIGH-LIFT WINGS IN CLOSED WIND TUNNELS Robert Glenn Joppa SUMMA... | USA | Total words: 22,736 | wind: 71 | tunnels: 23 | View |
| 344310.1 | Role of Computational Fluid Dynamics and Wind Tunnels in Aeronautics R&DPDF | wind-tunnel testing that was conducted during the same periodBecause computer speed is . expected to... | USA | Total words: 28,050 | wind: 154 | tunnels: 66 | View |
| 344310.1 | OVERVIEW OF THE 1989 WIND TUNNEL CALmRATION Wom,:sI-IOI,PDF | ultimate goal of developing wind tunnel calibration requirements for the major NASA wind tunnels at ... | USA | Total words: 3,565 | wind: 4 | tunnels: 1 | View |
| 344310.1 | The George C. Marshall Space Flight Center's 14 X 14-Inch Trisonic Wind ... | A history of the National Aeronautics and Space Administration (NASA) George C. Marshall Space Fligh... | USA | Total words: 383 | wind: 7 | tunnels: 1 | View |
| 344310.1 | I 1 JOINT INSTITUYE FOR AERONAUTICS AND ACOUSTICS 7 &/O 3PDF | low-speed wind tunnels was that due to Bradshaw and Pankhurst (1964). However, re- cent experimental... | USA | Total words: 9,221 | wind: 55 | tunnels: 19 | View |
| 344310.1 | 14- by 22-Foot Subsonic Wind Tunnel - NASA | The 14- by 22-Foot Subsonic Wind Tunnel assesses conventional performance for low-speed tests of pow... | USA | Total words: 1,375 | wind: 11 | tunnels: 1 | View |
| 344310.1 | WIND TUNNEL MODEL SYSTEMS CRITERIA - NASAPDF | The Wind Tunnel Model Systems Committee, as outlined in LAPD 1150.2 has ownership of this document. ... | USA | Total words: 19,462 | wind: 39 | tunnels: 5 | View |
| 344310.1 | Publication - USDA ARS | Wind tunnel use for UAV applications was spray drift centric for UAV variables such as rotor configu... | USA | Total words: 693 | wind: 12 | tunnels: 6 | View |
| 344310.1 | N/ SAPDF | For most wind-tunnel test planning, Margason (Ref. 5) has provided an excellent checklist defining t... | USA | Total words: 9,656 | wind: 18 | tunnels: 4 | View |
| 344310.1 | The Next Generation of High-Speed Dynamic Stability Wind Tunnel Testing ...PDF | the TDT utilizing the same wind tunnel model; one test with the legacy system and the other with the... | USA | Total words: 6,081 | wind: 16 | tunnels: 2 | View |
| 344310.1 | Static Aeroelastic Modeling of a Sub-Scale Wind Tunnel Model with Novel ...PDF | Figure 5. UWAL Wind Tunnel Model VCCTEF Dimensions (Courtesy of UWAL) Figure 6. UWAL Wind Tunnel Mod... | USA | Total words: 9,471 | wind: 121 | View |
| 344310.1 | 11-Foot Transonic Unitary Plan Facility (11×11) - NASA | This wind tunnel has set a new standard in test productivity and technical excellence. The 11- by 11... | USA | Total words: 1,355 | wind: 10 | tunnels: 1 | View |
| 344310.1 | Application of Pressure-Based Wall Correction Methods to Two NASA ...PDF | The two NASA LaRC tunnels extensively employed for subsonic and transonic testing of transport and f... | USA | Total words: 2,858 | wind: 5 | tunnels: 5 | View |
| 344310.1 | 8- by 6-Foot Supersonic Wind Tunnel Facility - NASA | The 8′ x 6′ Supersonic Wind Tunnel operates either in an aerodynamic closed-loop cycle, testing ... | USA | Total words: 1,466 | wind: 21 | tunnels: 2 | View |
Page 10 of 49 (976 records)