Development of analytical and experimental techniques for the determination of distributed loads on stores
Author:
Affiliation:
1. Calspan Field Services, Inc., Arnold Air Force Station, TN
2. USAF, Armament Laboratory, Elgin AFB, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1896
Reference12 articles.
1. 2Kcilock, Robert E. and Miller, Percy H. "Aerodynamic Characteristics of Basic Nose-Cylinder Bodies for Large Ranges of Anglc of Attack,'' 1,ouisianaState University, 1971.
2. An experimental technique was developed to measurc load distributions on stores in a wind tunnel by using a segmented model with separate balanccs for each segment. The validity of the tcchnique was cstablished by comparing the data from a large-scale four-scgmcntmodel with data from a large-scalcpressure model and was extended to a smaller scale using a three-segmentmodel of the samc configuration. A small-scalesegmented model will be tested in the carriage position on an aircraft, providing data for validation of the interfcrcnce flow-field distributed loads prediction techniquc. "Acrodyiamic Methodology (Isolated'Fins and Bodies),'' Martin Marietta Corporation OR 12,399,March 1973.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Historical perspective on the integration of testing and evaluation methodologies at the Arnold Engineering Development Center;25th Plasmadynamics and Lasers Conference;1994-06-20
2. New approaches to computational aircraft/store weapons integration;28th Aerospace Sciences Meeting;1990-01-08
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