TY - JOUR
AB - In combination with an aircraft, a receptacle having a perforate side and imperforate other sides, said perforate side being composed of a surface portion of said aircraft, a muffleer in said receptacle a compartment scaled, spaced from, and partially enclosing said receptacle, said compartment having a perforate wall and imperforate other walls, said perforate wall of said compartment forming a part of the surface of said aircraft which lies between said perforate side of said receptacle and the adjacent surfaces of said aircraft, and means to circulate a cooling medium through said chamber.
TI - U.S. Patent Specifications
JF - Aircraft Engineering and Aerospace Technology
DO - 10.1108/eb030306
DA - 1938-04-01
UR - https://www.deepdyve.com/lp/emerald-publishing/u-s-patent-specifications-mZZIBl8nRu
SP - 124
EP - 124
VL - 10
IS - 4
DP - DeepDyve
ER -