Download Free A Tabulation Of Wind Tunnel Pressure Data And Section Aerodynamic Characteristics At Mach Numbers Of 161 And 201 For Two Trapezoidal And Three Delta Wings Having Different Surface Shapes Book in PDF and EPUB Free Download. You can read online A Tabulation Of Wind Tunnel Pressure Data And Section Aerodynamic Characteristics At Mach Numbers Of 161 And 201 For Two Trapezoidal And Three Delta Wings Having Different Surface Shapes and write the review.

Pressure data have been obtained in the Langley 8-foot transonic tunnel at Mach numbers from 0.80 to 1.115 and angles of attack from 0 to 20 degrees for wing-body configurations employing a thin trapezoidal wing in combination with basic and indented bodies. The wing had 26.6 degrees sweepback of the quarter-chord line, an aspect ratio of 2.61, a taper ratio of 0.211, and 2-percent-thick symmetrical circular-arc airfoil sections parallel to the plane of symmetry. Results are also presented for the basic body alone. Reynolds numbers for the tests were on the order of 2,600,000, based on the wing mean aerodynamic chord.