By Joslin, Ronald D.; Jones, Gregory S.(eds.)
In keeping with papers from the 2004 NASA/ONR stream regulate Workshop, this assortment is a useful, distinct source at the cutting-edge in movement keep an eye on applied sciences and purposes. Filling the data hole among 1986, while the final such symposium was once held, and this present day, it summarizes the purposes, experiments, computations and theories relating to circulate regulate, emphasizing basic physics, platforms research and utilized study. The papers provided conceal a large choice of aerodynamic and hydrodynamic functions together with; naval automobiles, fixed-wing aviation, V/STOL structures, propulsion structures, and floor vehicles.
- facts and data showing during this booklet are for informational reasons basically. AIAA and the writer usually are not accountable for any damage or harm due to use or reliance, nor do AIAA and the writer warrant that use or reliance can be loose from privately owned rights.
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Extra info for Applications of Circulation Control Technologies
The solid lines represent the portion of either the inner or outer slot that is open and where the fluid ejection occurs. The author suggests reviewing Table 3 before reading further. As a simple illustration of force vectoring capability, a long strand of yam was positioned in the center of the CC-Duct. The photograph on the left of Fig. 16 shows the configuration with no CC blowing. The yam is aligned with the tunnel free stream velocity, along the longitudinal axis of the Duct. The photograph on the right of Fig.
21 CCW/Supercritical, dual-radius CCW, and conventional mechanical flap airfoil comparisons. 42 R. J. ENGLAR Fig. 22 Low-speed drag polars for CCW/Supercritical airfoil. LIVE GRAPH Freedream Mach Amber, Iy, Click here to view Fig. ' OVERVIEW OF CC PNEUMATIC AERODYNAMICS 43 Supercritical Contour Fig. 24 Dual radius CCW airfoil with LE blowing. For the 90-deg flap shown here, the jet turning angle is about 135 deg (compare to Figs. 8 and lo), limited by the TE comer. With flap retracted to 0 deg, the airfoil is in a sharp-TE cruise configuration.
2 Cross-section of LSB airfoil! Lower Surface Blowing (LSB) Slot R. IMBER, E. ROGERS, AND J. ABRAMSON 72 ACr due to blowing LIVE GRAPH Click here to view Momentum Coefficient, Cp Fig. 3 Comparison of lift performance for dual-slotted LSB and single-slot parent airfoil? against momentum coefficient, and reveals that the goal of doubling the control range was met. An unanticipated finding was that the performance of the lower slot, in terms of measured lift augmentation ratio, was noticeably better than that for the upper slot (80 compared with 60).