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A methodology for designing aircraft to low sonic boom constraints
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Needleman, Kathy E. Mack, Robert J. |
| Copyright Year | 1991 |
| Description | A method for designing conceptual supersonic cruise aircraft to meet low sonic boom requirements is outlined and described. The aircraft design is guided through a systematic evolution from initial three view drawing to a final numerical model description, while the designer using the method controls the integration of low sonic boom, high supersonic aerodynamic efficiency, adequate low speed handling, and reasonable structure and materials technologies. Some experience in preliminary aircraft design and in the use of various analytical and numerical codes is required for integrating the volume and lift requirements throughout the design process. |
| File Size | 3693412 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910008792 |
| Archival Resource Key | ark:/13960/t25b5161t |
| Language | English |
| Publisher Date | 1991-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Supersonic Aircraft Noise Reduction Low Speed Propulsive Efficiency Controllability Mathematical Models Aircraft Design Sonic Booms Aerodynamic Characteristics Lift Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
