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Title: Noise and sonic-boom impact technology. PCBOOM computer program for sonic-boom research. Volume 1. Technical report. Final report, May 1987-October 1988

Technical Report ·
OSTI ID:5925042

The PCBOOM computer program, described in this technical report, calculates the location and magnitude of sonic-boom overpressures on the ground due to supersonic flight under standard atmosphere and no wind-propagation conditions. The program is intended for environmental planners and engineers who may need to estimate the noise impact from individual flights of supersonic military aircraft. The program runs on a Zenith Z-248 personal computer and also should run on most similarly configured IBM-compatible computers. The program contains information for all current military aircraft and allows updating for additional aircraft. The user can select either 'Quick look' computations which assume steady-state flight or detailed ray-tracing calculations which can handle non-steady flight and sonic-boom focus conditions. Several types of simple maneuvers can be selected for computations; the program will also handle up to ten connected straight-line segments. Flight segments from the MOAOPS library of supersonic combat training flights may also be selected. User-specified output for printer, plotter or screen includes tables of overpressures and graphic display of the sonic-boom overpressure 'footprints' on the ground. The footprint plots show the location of all ray positions that exceed overpressures of a given level. Flight track, Mach number, and altitude profile plots are also provided. This report summarizes the technical basis for PCBOOM. Two other reports provide a program users/computer operations manual and a program maintenance manual.

Research Organization:
BBN Labs., Inc., Canoga Park, CA (USA)
OSTI ID:
5925042
Report Number(s):
AD-A-206290/9/XAB; BBN-6741-VOL-1
Resource Relation:
Other Information: See also Volume 2, AD-A206 291
Country of Publication:
United States
Language:
English