1. Structural acoustic response, noise transmission losses, and interior noise levels of an aircraft fuselage excited by random pressure fields;Cockburn;Air Force Flight Dynamic Laboratory, Technical Report, AFFDC-TR-68-2,1968
2. Effect of air flow, panel curvature and internal pressurization on field incidence transmission loss;Koval;Journal of the Acoustical Society of America,1976
3. On sound transmission into a thin cylindrical shell under “flight conditions”;Koval;Journal of Sound and Vibration,1976
4. Reduction of cabin noise by fuselage structural optimization;Bhat,1977
5. Analytical study of interior noise control by fuselage design techniques on high-speed, propeller driven aircraft;Revell;NASA CR-159222,1978