SY T 7472-2020 油气管道完整性管理等级评估规范.pdf

相关资源

SY T 6784-2023 钢质储罐腐蚀控制技术规范.pdf

SY T 7686-2023 储气库库存评价技术规范.pdf

SY T 7695-2023 石油工业标准化文件的俄文译本通用表述.pdf

SY T 7675-2022 天然气 水露点和烃露点的测定 偏振光冷镜法.pdf

SY T 7684-2023 大型立式圆筒形钢制焊接储罐检测技术规范.pdf

SY T 7691-2023 盐穴型储气库地面工程设计规范.pdf

SY T 7677-2023 湿陷性黄土地区石油天然气工程设计规范.pdf

SY T 7671-2022 加油加气站信息系统建设技术规范.pdf

SY T 7687-2023 气藏型储气库动态分析技术规范.pdf

SY T 7689-2023 盐穴储气库腔体设计技术要求.pdf

猜你喜欢

NASA NACA-RM-A51D25-1951 Low-speed characteristics of a wing having 63 degrees sweepback and uniform camber《带有63后掠角和均匀弧度的机翼低速特性》.pdf

NASA NACA-RM-A51D27-1951 Characteristics throughout the subsonic speed range of a plane wing and of a cambered and twisted wing both having 45 degrees of sweepback《拱形和扭转机翼的飞机机翼(均有4.pdf

NASA NACA-RM-A51G31-1951 The forces and pressure distribution at subsonic speeds on a plane wing having 45 degrees of sweepback an aspect ratio of 3 and a taper ratio of 0 5《在亚音速下 .pdf

NASA NACA-RM-A51H02-1951 Lift drag and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds - plane triangular wing of aspect ratio 3 with NACA 0003-63 secti.pdf

NASA NACA-RM-A51J11-1951 The effects at transonic speeds of thickening the trailing edge of a wing with a 4-percent-thick circular-arc airfoil《在跨音速下 将带有4%厚度圆弧机翼的机翼后缘增厚的效果》.pdf

NASA NACA-RM-A51L03-1952 Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 2 triangular wing and an all-movable horizontal tail latera.pdf

NASA NACA-RM-A52B20-1952 The effects of Reynolds number at Mach numbers up to 0 94 on the loading on a 35 degree swept-back wing having NACA 65(1)A012 streamwise sections《在马赫数达到0 9.pdf

NASA NACA-RM-A52D22-1952 The forces and pressure distribution at subsonic speeds on a cambered and twisted wing having 45 degrees of sweepback and aspect ratio of 3 and a taper rat.pdf

NASA NACA-RM-A52F18-1952 The longitudinal characteristics at Mach numbers up to 0 92 of a cambered and twisted wing having 40 degrees of sweepback and an aspect ratio of 10《在马赫数达到0.pdf