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| Measurement of the steady surface pressure distribution on a single rotation large scale advanced prop-fan blade at Mach numbers from 0.03 to 0.78 科技报告
报告编号: NASA-CR-182124, E-4137, NAS 1.26:182124. 出版年: 1988
作者: Bushnell, Peter
  收藏 | 浏览/下载：7/0 | 提交时间：2019/11/30
COMPUTATIONAL FLUID DYNAMICS PRESSURE DISTRIBUTION PROP-FAN TECHNOLOGY ROTOR BLADES (TURBOMACHINERY) STRUCTURAL DESIGN AERODYNAMIC CONFIGURATIONS GRAPHS (CHARTS) MACH NUMBER TABLES (DATA) WIND TUNNEL TESTS |
| Investigation to optimize the passive shock wave-boundary layer control for supercritical airfoil drag reduction 科技报告
报告编号: NASA-CR-173276, NAS 1.26:173276. 出版年: 1983
作者: Nagamatsu, H. T.; Ficarra, R.; Orozco, R.
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BOUNDARY LAYER CONTROL DRAG REDUCTION SHOCK WAVES SUPERCRITICAL WINGS MACH NUMBER POROSITY PRESSURE DISTRIBUTION SCHLIEREN PHOTOGRAPHY STATIC PRESSURE TRANSONIC WIND TUNNELS |
| A method to estimate weight and dimensions of small aircraft propulsion gas turbine engines: User's guide 科技报告
报告编号: NASA-CR-168049, NAS 1.26:168049, GARRETT-21-4270-1.1. 出版年: 1982
作者: Hale, P. L.
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AIRCRAFT ENGINES GAS TURBINE ENGINES SIZE (DIMENSIONS) STRUCTURAL WEIGHT COMPUTER PROGRAMS ENGINE PARTS HEAT EXCHANGERS MACH NUMBER |
| Calculations of the Supersonic Wave Drag of Nonlifting Wings with Arbitrary Sweepback and Aspect Ratio: Wings Swept Behind the Mach Lines 科技报告
报告编号: NACA-RM-L6K29. 出版年: 1947
作者: Harmon, Sidney M; Swanson, Margaret D
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AERODYNAMIC DRAG SWEPTBACK WINGS SUPERSONIC DRAG ASPECT RATIO AERODYNAMIC COEFFICIENTS SUPERSONIC SPEED MACH NUMBER LEADING EDGES |
| Investigation of Diving Moments of a Pursuit Airplane in the Ames 16-Foot High Speed Wind Tunnel 科技报告
报告编号: NACA-WR-A-65. 出版年: 1942
作者: Erickson, Albert L
收藏 | 浏览/下载：11/0 | 提交时间：2019/11/30
SUBSONIC SPEED FUSELAGES AIRCRAFT MODELS MANEUVERABILITY FLIGHT CONTROL AIRCRAFT MANEUVERS MACH NUMBER SCALE MODELS TRANSONIC WIND TUNNELS |
