Static Aerodynamic Characteristics, Pressure Distributions, and RAM-air Inflation of Attached Inflatable Decelerator Models at Mach 3.0

· National Aeronautics and Space Administration
电子书
59
页

关于此电子书

Static aerodynamic characteristics, pressure distributions, and ram air inflation of attached inflatable drag chute models at supersonic speed.

为此电子书评分

欢迎向我们提供反馈意见。

如何阅读

智能手机和平板电脑
只要安装 Android 和 iPad/iPhone 版的 Google Play 图书应用，不仅应用内容会自动与您的账号同步，还能让您随时随地在线或离线阅览图书。
笔记本电脑和台式机
您可以使用计算机的网络浏览器聆听您在 Google Play 购买的有声读物。
电子阅读器和其他设备
如果要在 Kobo 电子阅读器等电子墨水屏设备上阅读，您需要下载一个文件，并将其传输到相应设备上。若要将文件传输到受支持的电子阅读器上，请按帮助中心内的详细说明操作。

William D. Deveikis的更多图书

Local Aerodynamic Heat Transfer and Boundary-layer Transition on Roughened Sphere-ellipsoid Bodies at Mach Number 3.0
William D. Deveikis
免费
Investigation of the Compressive Strength and Creep of 7075-T6 Aluminum-alloy Plates at Elevated Temperatures
William D. Deveikis
免费
Flow Patterns and Pressure Distributions Around a Bluff Afterbody in the Wake of a 120° Cone for Various Separation Distances at Mach 3.0
William D. Deveikis
免费
Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack: Subsonic, Transonic, and Supersonic Speeds, Issues 1301-1310
A. Gerald Rainey
免费

类似电子书

Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack: Subsonic, Transonic, and Supersonic Speeds, Issues 1301-1310
A. Gerald Rainey
免费