EFFECTS OF WING-TIP VORTICES AND SONIC SHOCK ON ARMY AIRCRAFT IN FLIGHT Open PDF Document Details Document Type Technical Report Publication Date May 01, 1957 Accession Number AD0134995 Tags Communities of Interest Air Platforms DTIC Thesaurus Topics Air Force Aircraft Equipment Aircraft Landings Aircrafts Airframes Commercial Aircraft Commercial Pilots Engineering Engineers Jet Aircraft Measurement Shock Waves Sonic Boom Time Intervals Transport Aircraft United States Wind Velocity