Andere Kunden interessierten sich auch für
![System Lightweight Design for Aviation]( "System Lightweight Design for Aviation")
System Lightweight Design for Aviation30,99 €![Gyroless Attitude Determination of Nanosatellites]( "Gyroless Attitude Determination of Nanosatellites")
Gyroless Attitude Determination of Nanosatellites42,99 €![Evaluating Accuracy Measures for Flight Delay Predictions: Minimizing]( "Evaluating Accuracy Measures for Flight Delay Predictions: Minimizing")
Evaluating Accuracy Measures for Flight Delay Predictions: Minimizing29,99 €![Optimized Controller for Attitude and Orbit Determination and Control]( "Optimized Controller for Attitude and Orbit Determination and Control")
Optimized Controller for Attitude and Orbit Determination and Control32,99 €![Efficient Pressure Load Transfer]( "Efficient Pressure Load Transfer")
Efficient Pressure Load Transfer36,99 €![From Data Modeling to Knowledge Engineering in Space System Design]( "From Data Modeling to Knowledge Engineering in Space System Design")
From Data Modeling to Knowledge Engineering in Space System Design60,00 €![Application of Surrogate-based Global Optimization to Aerodynamic Design]( "Application of Surrogate-based Global Optimization to Aerodynamic Design")
Application of Surrogate-based Global Optimization to Aerodynamic Design74,99 €
The present work delivers a versatile, accurate and reliable wind tunnel facility that is particularly developed to test different flow control techniques for drag reduction in precisely adjustable test conditions. Skin friction changes of 0.4% are resolved, which is comparable to the most accurate reported studies in liquids. this high accuracy is verified through a comprehensive uncertainty analysis. Subsequently, various passive and active flow control strategies are investigated.