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| An adaptive finite element method for high speed compressible flow 科技报告
报告编号: NASA-CR-173443, NAS 1.26:173443, C/R/479/84. 出版年: 1984
作者: Loehner, R.; Morgan, K.; Zienkiewicz, O. C.
  收藏 | 浏览/下载：13/0 | 提交时间：2019/11/30
COMPRESSIBLE FLOW FINITE ELEMENT METHOD HIGH SPEED PRANDTL-MEYER EXPANSION WEDGE FLOW ALGORITHMS COMPUTATIONAL FLUID DYNAMICS COMPUTATIONAL GRIDS DOMAINS FLUID FLOW NUMERICAL ANALYSIS SUPERSONIC FLOW WEDGES |
| Heat transfer tests of an 0.006-scale thin-skin space shuttle thermocouple model (41-OTS) in the Langley Research Center unitary plan wind tunnel at M equals 3.7 (IH16) 科技报告
报告编号: NASA-CR-141534, DMS-DR-2166. 出版年: 1975
作者: Walstad, D. G.
收藏 | 浏览/下载：10/0 | 提交时间：2019/11/30
SPACE SHUTTLE ASCENT STAGE SPACE SHUTTLES SUPERSONIC HEAT TRANSFER WIND TUNNEL TESTS AERODYNAMIC HEATING EXTERNAL TANKS GRAPHS (CHARTS) SPACE SHUTTLE BOOSTERS SPACECRAFT CONFIGURATIONS SPACECRAFT MODELS SUPERSONIC SPEED TABLES (DATA) THERMOCOUPLES |
| A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow 科技报告
报告编号: NACA-TR-1052. 出版年: 1951
作者: Jones, Arthur L; Alksne, Alberta
收藏 | 浏览/下载：11/0 | 提交时间：2019/11/30
AIRCRAFT AERODYNAMIC STABILITY AIRCRAFT STABILITY LATERAL STABILITY THIN WINGS SUPERSONIC SPEED PLANFORMS COMPRESSIBILITY EFFECTS STABILITY DERIVATIVES COMPUTATIONAL FLUID DYNAMICS TRAPEZOIDAL WINGS RECTANGULAR WINGS SWEPTBACK WINGS DELTA WINGS DESIGN CHARTS |
| An Approximate Method of Calculating Pressures in the Tip Region of a Rectangular Wing of Circular-Arc Section at Supersonic Speeds 科技报告
报告编号: NACA-TN-2211. 出版年: 1950
作者: Czarnecki, Kazimierz Roman; Mueller, James N
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PRESSURE DISTRIBUTION WING TIPS RECTANGULAR WINGS SUPERSONIC SPEED APPROXIMATION |
| 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
收藏 | 浏览/下载：13/0 | 提交时间：2019/11/30
AERODYNAMIC DRAG SWEPTBACK WINGS SUPERSONIC DRAG ASPECT RATIO AERODYNAMIC COEFFICIENTS SUPERSONIC SPEED MACH NUMBER LEADING EDGES |
