Sponsored by theFluid Dynamics Panel of AGARD.
|Series||Agard advisory reports -- 318|
|Contributions||Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel.|
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This banner text can have markup.. web; books; video; audio; software; images; Toggle navigation. American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Moving Surface Boundary-layer Control (MSBC) was applied to several two dimensional bluff bodies using a high speed rotating cylinder as a momentum injecting device. Flow past a symmetric airfoil; a D-section; as well as square and rectangular prisms, representing a family of shapes with progressively increasing bluffness were studied in presence of the MSBC. In the case of the airfoil, the Cited by: 2. Items where Subject is "AERONAUTICS > Aerodynamics" NB and Viswanath, PR () Drag Reduction from Square-Base Afterbodies at High Speeds. Journal of Aircraft, 41 (4). pp. Computations with 3-D Euler code for wings. Journal of Aeronautical Society of India, pp. Sundaram, S and Vishwanath.