Study Covering Calculations and Analysis of Sonic Boom during Operational Maneuvers. Volume I. Analysis and Computation of Maneuver Effects.

Abstract

The methods and results of the study of the effects of operational SST maneuvers on sonic boom are contained in three volumes. Volume I shows that the theoretical effects of operational maneuvers due to typical SST maneuvers are small except for maneuvers at Mach numbers below about Mach 1.3. Methods are outlined for applying the results to any airplane, and selected pressure signatures are presented for the U.S. SST and SCAT 15-F. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1971
Accession Number
AD0735296

Entities

Organizations

  • Boeing Commercial Airplanes

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Computations
  • Coverings
  • Fixed Wing Aircraft
  • Mach Number
  • Maneuvers
  • Pressure Signatures
  • Sonic Boom
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Combustion and Flow Dynamics.
  • Maritime Combat Support and Expeditionary Logistics.