The combined load statistics are developed by taking the acoustically induced load to be a random population, assumed to be stationary. Each element of this ensemble of acoustically induced loads is assumed to have the same power spectral density (PSD), obtained previously from a random response analysis employing the given acoustic field in the STS cargo bay as a stationary random excitation. The mechanically induced load is treated as either (1) a known deterministic transient, or (2) a nonstationary random variable of known first and second statistical moments which vary with time. A method is then shown for determining the probability that the combined load would, at any time, have a value equal to or less than a certain level. Having o...
Scaling fluctuating pressure environments for high performance aerospace vehicles in acoustic design...
A high frequency random vibration analysis, (statistical energy analysis (SEA) method) is examined. ...
A method for calculating the aerodynamic loading on a wing in combination with a body is presented. ...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
The single axis acoustic levitator that was flown on SPAR VI malfunctioned. The results of a series ...
Random numbers were generated with the aid of a digital computer and transformed such that the proba...
This report is an aid to designers of structures with large area-to-mass ratios that are subject to ...
This paper presents a deterministic theory for the random vibration problem for predicting the respo...
During liftoff and ascent flight phases, the Space Transportation System (STS) and payloads are expo...
A review of the acoustic fatigue design process for aircraft structures is presented in this paper, ...
Information on probabilistic structural analysis methods for space propulsion systems is given in vi...
Data presented from large-scale model tests with jet engines having thrusts of 9 kN (2000 lb) and 36...
External acoustic environments, structural responses, noise reductions, and the internal acoustic en...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
Scaling fluctuating pressure environments for high performance aerospace vehicles in acoustic design...
A high frequency random vibration analysis, (statistical energy analysis (SEA) method) is examined. ...
A method for calculating the aerodynamic loading on a wing in combination with a body is presented. ...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
The single axis acoustic levitator that was flown on SPAR VI malfunctioned. The results of a series ...
Random numbers were generated with the aid of a digital computer and transformed such that the proba...
This report is an aid to designers of structures with large area-to-mass ratios that are subject to ...
This paper presents a deterministic theory for the random vibration problem for predicting the respo...
During liftoff and ascent flight phases, the Space Transportation System (STS) and payloads are expo...
A review of the acoustic fatigue design process for aircraft structures is presented in this paper, ...
Information on probabilistic structural analysis methods for space propulsion systems is given in vi...
Data presented from large-scale model tests with jet engines having thrusts of 9 kN (2000 lb) and 36...
External acoustic environments, structural responses, noise reductions, and the internal acoustic en...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
Scaling fluctuating pressure environments for high performance aerospace vehicles in acoustic design...
A high frequency random vibration analysis, (statistical energy analysis (SEA) method) is examined. ...
A method for calculating the aerodynamic loading on a wing in combination with a body is presented. ...