RESPONSE OF STRUCTURES TO AIRCRAFT GENERATED SHOCK WAVES Open PDF Document Details Document Type Technical Report Publication Date Apr 01, 1959 Accession Number AD0229463 Tags Communities of Interest Air Platforms DTIC Thesaurus Topics Air Force Aircrafts Angle Of Incidence Construction Dynamic Pressure Dynamic Response Equations Flight Flow Materials Pressure Distribution Resonant Frequency Shock Waves Stagnation Pressure Static Pressure United States Vibration