Affiliation:
1. Pennsylvania State University
Publisher
American Institute of Aeronautics and Astronautics
Reference47 articles.
1. The Drag as Integral of the Entropy Flow
2. Maskell, E. C. “Progress Towards a Method for the Measurement of the Components of the Drag of a Wing of Finite Span,” Tech. Rep. 72232, Royal Aircraft Establishment, Procurement Executive, Ministry of Defence, 1972.
3. Shock Waves and Drag in the Numerical Calculation of Compressible, Irrotational Transonic Flow
Cited by
1 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