TY  - BOOK
AU  - Bennett, Floyd V.
TI  - Comparison of experimental and theoretical static aeroelastic loads and deflections of a thin 45 deg delta wing in supersonic flow [NASA TN D-974]
PY  - 1961///
PB  - Nasa, Washington, D.C.
KW  - Aeroelastic
N1  - Bound With Nasa Tn D-971-973,975-980; Technical Note D-974
ER  -