Supersonic Flow Field Visualization Studies of the M (infinity) = 6 Price Waverider Planform.

摘要

personic tests of the conical flow derived M(infinity) =6 (design) Price waverider planform were conducted using the Naval Postgraduate School wind tunnel, These tests are part of a continuing effort to study the characteristics of waverider configured vehicles, Two sting-mounted, flat-plate stainless-steel Price waverider planform models were utilized for testing in the NPS 4-inch by 4-inch cross section supersonic blowdown wind tunnel, Tests at Mach numbers of M 1,7, 2,8 and 4 were attempted but flowfleld studies were only completed at M(infinity) = 4.