Use of Active Learning to Design Wind Tunnel Runs for Unsteady Cavity Pressure Measurements
Author(s) -
Ankur Srivastava,
Andrew J. Meade
Publication year - 2014
Publication title -
international journal of aerospace engineering
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.361
H-Index - 22
eISSN - 1687-5974
pISSN - 1687-5966
DOI - 10.1155/2014/218710
Subject(s) - latin hypercube sampling , wind tunnel , transonic , sampling (signal processing) , scheme (mathematics) , computer science , measure (data warehouse) , flow (mathematics) , simulation , engineering , meteorology , aerospace engineering , mechanics , mathematics , data mining , physics , monte carlo method , aerodynamics , electrical engineering , statistics , mathematical analysis , filter (signal processing)
Wind tunnel tests to measure unsteady cavity flow pressure measurements can be expensive, lengthy, and tedious. In this work, the feasibility of an active machine learning technique to design wind tunnel runs using proxy data is tested. The proposed active learning scheme used scattered data approximation in conjunction with uncertainty sampling (US). We applied the proposed intelligent sampling strategy in characterizing cavity flow classes at subsonic and transonic speeds and demonstrated that the scheme has better classification accuracies, using fewer training points, than a passive Latin Hypercube Sampling (LHS) strategy
Accelerating Research
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom
Address
John Eccles HouseRobert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom