Measurements made in variable-density wind tunnel to determine pressure distribution over one section of R.A.F.-31 airfoil with leading edge slot fully open, to provide data for study of scale effect; tests conducted with air densities of approximately 1 and 20 atmospheres; full-scale maximum lift somewhat lower than maximum lift indicated by low scale.
Pressure distribution on a slotted R.A.F. 31 airfoil in the variable density wind tunnel
Nat. Advisory Committee Aeronautics -- Tech. Notes
1929
13 pages
12 Figs., Supp. plates, Bibliography
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.