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Aerobus: the aircraft of the future (basic problems of designing air buses)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sheynin, V. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1972 |
| Abstract | THE PROBLEMS ASSOCIATED WITH THE DESIGN OF AIR BUS TYPE AIRCRAFT ARE DISCUSSED. THE PRIMARY DESIGN PROBLEM IS IDENTIFIED AS THE SIZE AND WEIGHT OF THE AIRCRAFT. OTHER PROBLEMS INVOLVED IN THE AIRCRAFT CONFIGURATION ARE CONCERNED WITH THE CROSS SECTIONAL SHAPE OF THE FUSELAGE, THE LOCATION OF THE ENGINES, ACCOMMODATIONS FOR THE PASSENGERS, AND A COMPROMISE ON THE MAXIMUM CRUISE SPEED TO BE PERMITTED DURING OPERATION. THE RATIONALE BEHIND VARIOUS DECISIONS FOR THE AIR BUS DESIGN ARE EXPLAINED. |
| File Size | 498762 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19720016363 |
| Archival Resource Key | ark:/13960/t39z9w56c |
| Language | English |
| Publisher Date | 1972-05-01 |
| Access Restriction | Open |
| Subject Keyword | Systems Engineering Toroids Transformers Copper Iron Magnetic Cores Magnetic Flux Volt-ampere Characteristics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
