{"title":"导弹雷达罩超音速雨蚀试验","authors":"K. Barr, E. Steeger","doi":"10.2514/8.12440","DOIUrl":null,"url":null,"abstract":"S the advent of high speed aircraft and missiles, the damage to radomes and other parts from rain has become a problem requiring understanding and solution. Anticipating that this problem would become more important with increases in flight velocity, the materials laboratory of WADC sponsored a study of rain erosion testing techniques. One part of this study was undertaken by the Convair thermodynamics laboratories in 1952 and has continued since that time. A small group of engineers, under the direction of W. L. Dittmann, has been obtaining data on rain damage to radomes and radome materials at ever-increasing flight velocities. A large part of their task is to find methods that will accelerate the sample materials to high velocity without damage and with high probability of intact recovery. The first supersonic testing of materials was accomplished with a 20-mm aircraft cannon. Test specimens were mounted in the nose of a modified projectile and fired horizontally through 500 ft of simulated rainfall. Upon firing, a tracer element in the projectile was ignited and burned approximately f sec. A black powder charge then expelled the test specimen and parachute. The parachute checked the forward velocity of the test specimen within 10 ft and intact recovery was made. Speeds up to Mach 3.0 have thus been obtained. More recently, a 57-mm cannon was obtained. This increased the size of the test specimen to 2-in. diam. Data obtained from these studies show that erosion damage is a function of velocity, shape, material, water drop size and the distance the water drop must travel in the flow field aft of a shock. Thus, erosion damage obtained on an object with a 2-in. base diam will only simulate the damage to an equivalent nose portion of a corresponding larger specimen. The only method of obtaining quantitative results of rain damage to the total surface of a shape of much larger diameter is to test full scale. This was done by mounting fullscale radomes on a rocket sled and firing through a simulated rainfall.","PeriodicalId":304231,"journal":{"name":"Journal of Jet Propulsion","volume":"16 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2012-06-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Supersonic Rain Erosion Testing of Missile Radomes\",\"authors\":\"K. Barr, E. Steeger\",\"doi\":\"10.2514/8.12440\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"S the advent of high speed aircraft and missiles, the damage to radomes and other parts from rain has become a problem requiring understanding and solution. Anticipating that this problem would become more important with increases in flight velocity, the materials laboratory of WADC sponsored a study of rain erosion testing techniques. One part of this study was undertaken by the Convair thermodynamics laboratories in 1952 and has continued since that time. A small group of engineers, under the direction of W. L. Dittmann, has been obtaining data on rain damage to radomes and radome materials at ever-increasing flight velocities. A large part of their task is to find methods that will accelerate the sample materials to high velocity without damage and with high probability of intact recovery. The first supersonic testing of materials was accomplished with a 20-mm aircraft cannon. Test specimens were mounted in the nose of a modified projectile and fired horizontally through 500 ft of simulated rainfall. Upon firing, a tracer element in the projectile was ignited and burned approximately f sec. A black powder charge then expelled the test specimen and parachute. The parachute checked the forward velocity of the test specimen within 10 ft and intact recovery was made. Speeds up to Mach 3.0 have thus been obtained. More recently, a 57-mm cannon was obtained. This increased the size of the test specimen to 2-in. diam. Data obtained from these studies show that erosion damage is a function of velocity, shape, material, water drop size and the distance the water drop must travel in the flow field aft of a shock. Thus, erosion damage obtained on an object with a 2-in. base diam will only simulate the damage to an equivalent nose portion of a corresponding larger specimen. The only method of obtaining quantitative results of rain damage to the total surface of a shape of much larger diameter is to test full scale. 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引用次数: 2
摘要
随着高速飞机和导弹的出现,雨水对天线罩和其他部件的破坏已经成为一个需要理解和解决的问题。预料到这个问题会随着飞行速度的增加而变得更加重要,WADC的材料实验室赞助了一项关于雨蚀测试技术的研究。这项研究的一部分是由康维尔热力学实验室在1952年进行的,从那时起一直在继续。在w·l·迪特曼(W. L. Dittmann)的指导下,一小群工程师一直在获取在不断增加的飞行速度下雨水对雷达罩和雷达罩材料的损害的数据。他们的大部分任务是找到一种方法,使样品材料加速到高速而不损坏,并有很大的可能性完好无损地恢复。材料的第一次超音速测试是用一门20毫米机炮完成的。测试样本安装在一个改进的炮弹的前端,并在500英尺的模拟降雨中水平发射。在发射时,弹丸中的示踪元素被点燃并燃烧了大约5秒。然后黑色火药将测试样品和降落伞排出。降落伞在10英尺内检查了试样的前进速度,并进行了完整的回收。这样就获得了3.0马赫的速度。最近又获得了一门57毫米加农炮。这将测试样品的尺寸增加到2英寸。从这些研究中获得的数据表明,侵蚀损伤是速度、形状、材料、水滴大小和水滴在激波后流场中必须行进的距离的函数。因此,在一个2英寸的物体上得到侵蚀损伤。基础直径只能模拟对相应较大样本的等效鼻部部分的损伤。获得雨水对直径大得多的形状的总表面破坏的定量结果的唯一方法是进行全尺寸试验。这是通过在火箭雪橇上安装全尺寸的雷达罩并在模拟降雨中发射来完成的。
Supersonic Rain Erosion Testing of Missile Radomes
S the advent of high speed aircraft and missiles, the damage to radomes and other parts from rain has become a problem requiring understanding and solution. Anticipating that this problem would become more important with increases in flight velocity, the materials laboratory of WADC sponsored a study of rain erosion testing techniques. One part of this study was undertaken by the Convair thermodynamics laboratories in 1952 and has continued since that time. A small group of engineers, under the direction of W. L. Dittmann, has been obtaining data on rain damage to radomes and radome materials at ever-increasing flight velocities. A large part of their task is to find methods that will accelerate the sample materials to high velocity without damage and with high probability of intact recovery. The first supersonic testing of materials was accomplished with a 20-mm aircraft cannon. Test specimens were mounted in the nose of a modified projectile and fired horizontally through 500 ft of simulated rainfall. Upon firing, a tracer element in the projectile was ignited and burned approximately f sec. A black powder charge then expelled the test specimen and parachute. The parachute checked the forward velocity of the test specimen within 10 ft and intact recovery was made. Speeds up to Mach 3.0 have thus been obtained. More recently, a 57-mm cannon was obtained. This increased the size of the test specimen to 2-in. diam. Data obtained from these studies show that erosion damage is a function of velocity, shape, material, water drop size and the distance the water drop must travel in the flow field aft of a shock. Thus, erosion damage obtained on an object with a 2-in. base diam will only simulate the damage to an equivalent nose portion of a corresponding larger specimen. The only method of obtaining quantitative results of rain damage to the total surface of a shape of much larger diameter is to test full scale. This was done by mounting fullscale radomes on a rocket sled and firing through a simulated rainfall.