Accession Number:

AD0735296

Title:

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

Descriptive Note:

Final rept. Apr 70-Feb 71.

Corporate Author:

BOEING CO RENTON WASH COMMERCIAL AIRPLANE GROUP

Personal Author(s):

Report Date:

1971-02-01

Pagination or Media Count:

311.0

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

Subject Categories:

  • Acoustics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE