Quantitative low-speed wake surveys
- 1 March 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 31 (2) , 249-255
- https://doi.org/10.2514/3.46481
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Drag calculations of wings using Euler methodsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Evaluation of a Complete Wake Integral for the Drag of a Car-Like ShapeSAE International Journal of Advances and Current Practices in Mobility, 1984
- Drag Measurement Through Wake AnalysisSAE International Journal of Advances and Current Practices in Mobility, 1984
- Algorithm 541: Efficient Fortran Subprograms for the Solution of Separable Elliptic Partial Differential Equations [D3]ACM Transactions on Mathematical Software, 1979
- A generalized wake-integral approach for drag determination in three-dimensional flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Flow Survey of the Vortex Wake behind WingsJournal of Aircraft, 1977
- Computer-Controlled System for the Investigation of the Flow behind WingsJournal of Aircraft, 1977
- Effect of Simulated Jet Engines on the Flowfield behind a Swept-Back WingJournal of Aircraft, 1977
- Wind Tunnel Measurements of Rolling Moment in a Swept-Wing Vortex WakeJournal of Aircraft, 1976
- Axial flow in trailing line vorticesJournal of Fluid Mechanics, 1964