00584nam 2200157z- 450 9910712254303321(CKB)5470000002491579(EXLCZ)99547000000249157920230509c2018uuuu -u- -engNozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnelMoffett Field, CaliforniaNational Aeronautics and Space Administration, Ames Research CenterBOOK9910712254303321Nozzle plume3291285UNINA