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A practical low-boom overpressure signature based on minimum sonic boom theory
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Haglund, George T. Mack, Robert J. |
| Copyright Year | 1992 |
| Description | A brief resume of sonic boom minimization methods is given to provide a background for a new, empirical modification of the Seebass and George minimum-nose-shock sonic boom F-function and signature. The new 'hybrid' F-function has all the inherent flexibility of application found with the Darden-modified Seebass and George F-function. In addition, it has enhanced this flexibility and applicability with neglegible increase in nose and/or tail shock strength. A description of this 'hybrid' F-function and signature is provided, and the benefits of using them to design high-performance, low-boom aircraft are discussed. |
| File Size | 516609 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920076742 |
| Archival Resource Key | ark:/13960/t6wx29g31 |
| Language | English |
| Publisher Date | 1992-10-01 |
| Access Restriction | Open |
| Subject Keyword | Acoustics Shock Waves Overpressure Body-wing Configurations Noise Reduction Aircraft Noise Aircraft Performance Sonic Booms Signatures Optimization Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |