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| Effects of hole pitch variation on overall and internal effectiveness in the leading edge region of a simulated turbine blade with heat flux measurements 学位论文
出版年: 2010
作者: Dyson;Thomas Earl
  收藏 | 浏览/下载：10/0 | 提交时间：2019/11/29
Overall effectiveness Pitch variation Impingement cooling Relative curvature Concave Heat flux Angle of attack Turbine blade Leading edge Film cooling |
| Deformable wing kinematics in the desert locust: how and why do camber, twist and topography vary through the stroke? 期刊论文
发表期刊: JOURNAL OF THE ROYAL SOCIETY INTERFACE. 出版年: 2009, 卷号: 6, 期号: 38, 页码: 735-747
作者: Walker, Simon M.; Thomas, Adrian L. R.; Taylor, Graham K.
收藏 | 浏览/下载：5/0 | 提交时间：2019/11/28
kinematics photogrammetry angle of attack camber locust morphing |
| Recent developments in rotary-balance testing of fighter aircraft configurations at NASA Ames Research Center 科技报告
报告编号: NASA-TM-86714, REPT-85211, NAS 1.15:86714. 出版年: 1985
作者: Malcolm, G. N.; Schiff, L. B.
收藏 | 浏览/下载：7/0 | 提交时间：2019/11/30
AERODYNAMIC BALANCE AERODYNAMIC CONFIGURATIONS ANGLE OF ATTACK F-15 AIRCRAFT ROTARY STABILITY STABILITY TESTS REYNOLDS NUMBER SPIN STABILITY DERIVATIVES WIND TUNNEL TESTS |
| Aerodynamic results of a separation test (CA20) conducted at the Boeing transonic wind tunnel using 0.030-scale models of the configuration 140A/B (modified) SSV orbiter (model no. 45-0) and the Boeing 747 carrier (model no. AX 1319 I-1), volume 3. [wind tunnel tests] 科技报告
报告编号: NASA-CR-141846, DMS-DR-2217-VOL-3. 出版年: 1975
作者: Dziubala, T.; Esparza, V.; Gillins, R. L.; Petrozzi, M.
收藏 | 浏览/下载：10/0 | 提交时间：2019/11/30
BOEING 747 AIRCRAFT SCALE MODELS SPACE SHUTTLE ORBITERS TRANSONIC WIND TUNNELS WIND TUNNEL TESTS AERODYNAMIC CHARACTERISTICS ANGLE OF ATTACK PRESSURE DISTRIBUTION SIDESLIP STRAIN GAGES SUBSONIC SPEED TABLES (DATA) |
| Aerodynamics of the Fuselage 科技报告
报告编号: NACA-TM-1036. 出版年: 1942
作者: Multhopp, H.
收藏 | 浏览/下载：7/0 | 提交时间：2019/11/30
FUSELAGES MATHEMATICAL MODELS WIND TUNNEL TESTS AERODYNAMIC STABILITY NACELLES INCOMPRESSIBLE FLOW STRESS ANALYSIS STATIC STABILITY ANGLE OF ATTACK FORCE DISTRIBUTION BODY-WING AND TAIL CONFIGURATIONS ZERO LIFT |
| Pressure distribution over NACA 23012 airfoil with a slotted and a split flap 科技报告
报告编号: NACA-TR-718. 出版年: 1941
作者: Harris, Thomas A; Lowry, John G
收藏 | 浏览/下载：10/0 | 提交时间：2019/11/30
AIRFOILS AIRFOIL PROFILES WING FLAPS SPLIT FLAPS WING SLOTS PRESSURE DISTRIBUTION FORCE DISTRIBUTION WIND TUNNEL TESTS AERODYNAMIC LOADS CHORDS (GEOMETRY) ANGLE OF ATTACK PITCHING MOMENTS CENTER OF PRESSURE AERODYNAMIC COEFFICIENTS AIRCRAFT STRUCTURES AIRCRAFT DESIGN |
| Wind-tunnel research comparing lateral control devices, particularly at high angles of attack V : spoilers and ailerons on rectangular wings 科技报告
报告编号: NACA-TR-439. 出版年: 1933
作者: Weick, Fred E; Shortal, Joseph A
收藏 | 浏览/下载：8/0 | 提交时间：2019/11/30
AIRCRAFT CONTROL LATERAL CONTROL CONTROL SURFACES SPOILERS AILERONS RECTANGULAR WINGS WIND TUNNEL TESTS YAWING MOMENTS ROLLING MOMENTS AERODYNAMIC CHARACTERISTICS ANGLE OF ATTACK SIDESLIP SIZE (DIMENSIONS) POSITION (LOCATION) |
