Download Free Effects Of The Spanwise Chordwise And Vertical Location Of An External Store On The Aerodynamic Characteristics Of A 45 Degree Sweptback Tapered Wing Of Aspect Ratio 4 At Mach Numbers Of 141 162 And 196 Book in PDF and EPUB Free Download. You can read online Effects Of The Spanwise Chordwise And Vertical Location Of An External Store On The Aerodynamic Characteristics Of A 45 Degree Sweptback Tapered Wing Of Aspect Ratio 4 At Mach Numbers Of 141 162 And 196 and write the review.

An aerodynamic investigation has been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effects of taper-in-thickness on the aerodynamics characteristics of wings having 35 and 45 degrees of sweep-back, aspect ratio 6, and taper ratio 0.60. The wings were tapered from NACA 65A009 airfoil sections at the root chord to NACA 65A003 airfoil sections at the tip chord. The test Mach number range was from 0.60 to 1.14 at a Reynolds number of the order of 500,000.
A transonic investigation of the effects of sweepback and thickness ratio on the wing loads of a wing in the presence of a body has been made in the Langley 8-foot transonic pressure tunnel. The tests covered wings with a thickness ratio of 6 percent for sweepback angles of 0, 25, and 45 degrees and a thickness ratio of 4 percent for an unswept wing.