TY  - BOOK
AU  - Trimpi,Robert L
AU  - Cohen,Nathaniel B
TI  - A NONLINEAR THEORY FOR PREDICTING THE EFFECTS OF UNSTEADY LAMINAR, TURBULENT, OR TRANSITIONAL BOUNDARY LAYERS ON THE ATTENUATION OF SHOCK WAVES IN A SHOCK TUBE WITH EXPERIMENTAL COMPARISON
U1  - NASA 
PY  - 1961///
CY  - 
PB  - Nasa, Washington, D.C.
N1  - Bound With Nasa Tr R-81-84,86-90
ER  -