Random Noise and Vibration in Space Vehicles
Author : Richard H. Lyon
Publisher :
Page : 84 pages
File Size : 10,92 MB
Release : 1967
Category : Airplanes
ISBN :
Author : Richard H. Lyon
Publisher :
Page : 84 pages
File Size : 10,92 MB
Release : 1967
Category : Airplanes
ISBN :
Author : Richard H. Lyon
Publisher :
Page : 68 pages
File Size : 43,54 MB
Release : 1967
Category : Airplanes
ISBN :
Author : Richard H. Lyon
Publisher :
Page : 80 pages
File Size : 16,18 MB
Release : 1967
Category : Airplanes
ISBN :
Author : J. Jaap Wijker
Publisher : Springer
Page : 516 pages
File Size : 27,12 MB
Release : 2009-08-29
Category : Technology & Engineering
ISBN : 9789048127290
Random Vibration in Spacecraft Structures Design is based on the lecture notes "Spacecraft structures" and "Special topics concerning vibration in spacecraft structures" from courses given at Delft University of Technology. The monograph, which deals with low and high frequency mechanical, acoustic random vibrations is of interest to graduate students and engineers working in aerospace engineering, particularly in spacecraft and launch vehicle structures design.
Author : Harry Himelblau
Publisher :
Page : 148 pages
File Size : 30,98 MB
Release : 1970
Category : Aerodynamic noise
ISBN :
This document provides a general survey of the field of space-vehicle structural vibration induced by acoustic and aerodynamic noise and certain mechanical excitation.
Author : Jaap Wijker
Publisher : Springer
Page : 229 pages
File Size : 12,54 MB
Release : 2018-01-25
Category : Technology & Engineering
ISBN : 3319731149
This book discusses the theory, applicability and numerous examples of Miles’ equation in detail. Random vibration is one of the main design drivers in the context of the design, development and verification of spacecraft structures, instruments, equipment, etc, and Miles’ equation provides a valuable tool for solving random vibration problems. It allows mechanical engineers to make rapid preliminary random response predictions when the (complex) structure is exposed to mechanical and acoustical loads. The book includes appendices to support the theory and applications in the main chapters.
Author : J. Jaap Wijker
Publisher : Springer Science & Business Media
Page : 517 pages
File Size : 47,38 MB
Release : 2009-08-19
Category : Technology & Engineering
ISBN : 9048127289
Random Vibration in Spacecraft Structures Design is based on the lecture notes "Spacecraft structures" and "Special topics concerning vibration in spacecraft structures" from courses given at Delft University of Technology. The monograph, which deals with low and high frequency mechanical, acoustic random vibrations is of interest to graduate students and engineers working in aerospace engineering, particularly in spacecraft and launch vehicle structures design.
Author : Alan D. Scott
Publisher :
Page : 136 pages
File Size : 14,39 MB
Release : 1996-06-01
Category :
ISBN : 9781423580898
The US space industry has accumulated a vast amount of expertise in the testing of spacecraft to ensure these vehicles can endure the harsh environments associated with launch and on-orbit operations. Even with this corporate experience, there remains a wide variation in the techniques utilized to test spacecraft during the development and manufacturing process, particularly with regard to spacecraft level dynamics testing. This study investigates the effectiveness of sinusoidal vibration, random vibration, acoustic noise and transient methods of spacecraft dynamic testing. An analysis of test failure and on-orbit performance data for acceptance testing indicates that the acoustic test is the most perceptive workmanship screen at the vehicle level and that additional dynamics tests do not result in an increase in acceptance test effectiveness. For spacecraft qualification, acoustic testing is almost universally employed for qualification in the high frequency environment. For the low frequency environment, data collected from a variety of spacecraft test programs employing sinusoidal sweep, random vibration and transient testing methods shows that a transient base excitation provides the most accurate simulation for the purpose of design verification. Furthermore, data shows that sinusoidal vibration testing provides an unrealistic simulation of the flight environment and results in an increased potential for overtesting.
Author : Robert A. Schiffer
Publisher :
Page : 7 pages
File Size : 35,24 MB
Release : 1964
Category : Aerodynamics, Transonic
ISBN :
Author : Harry Himelblau
Publisher :
Page : 148 pages
File Size : 39,86 MB
Release : 1970
Category : Aerodynamic noise
ISBN :
This document provides a general survey of the field of space-vehicle structural vibration induced by acoustic and aerodynamic noise and certain mechanical excitation.