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- [2] INFLUENCE OF SHOCK AND BOUNDARY LAYER INTERACTION ON SHOCK TUBE FLOWS BULLETIN OF THE AMERICAN PHYSICAL SOCIETY, 1968, 13 (05): : 785 - &
- [3] INFLUENCE OF SHOCK-WAVE ATTENUATION BY BOUNDARY-LAYER GROWTH ON CONTACT-SURFACE MOTION IN A SHOCK TUBE JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (06): : 388 - 389
- [6] INFLUENCE OF SHOCK-WAVE ATTENUATION BY BOUNDARY-LAYER GROWTH ON CONTACT-SURFACE MOTION IN A SHOCK TUBE - COMMENT JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (02): : 164 - 164
- [8] SHOCK TUBE TEST DURATION AND WALL BOUNDARY LAYER TRANSITION BEHIND STRONG SHOCK WAVES AIR BULLETIN OF THE AMERICAN PHYSICAL SOCIETY, 1968, 13 (05): : 796 - +