Yayın: Approximate solutions of range for constant altitude – constant high subsonic speed flight of transport aircraft
| dc.contributor.author | Aydan Cavcar | |
| dc.contributor.author | Cavcar, Aydan | |
| dc.contributor.author | Mustafa Cavcar | |
| dc.contributor.author | Cavcar, Mustafa | |
| dc.date.accessioned | 2025-11-13T10:31:35Z | |
| dc.date.issued | 2004-05-13 | |
| dc.identifier.doi | 10.1016/j.ast.2004.04.002 | |
| dc.identifier.endpage | 567 | |
| dc.identifier.issn | 1270-9638 | |
| dc.identifier.issue | 6 | |
| dc.identifier.openalex | W2025446950 | |
| dc.identifier.scopus | 2-s2.0-4243069396 | |
| dc.identifier.startpage | 557 | |
| dc.identifier.uri | https://hdl.handle.net/11421/4429 | |
| dc.identifier.uri | https://doi.org/10.1016/j.ast.2004.04.002 | |
| dc.identifier.volume | 8 | |
| dc.identifier.wos | 000223912000010 | |
| dc.language.iso | en | |
| dc.relation.ispartof | Aerospace Science and Technology | |
| dc.rights | restrictedAccess | |
| dc.subject | Cruise | |
| dc.subject | Aerospace engineering | |
| dc.subject | Mach number | |
| dc.subject | Constant (computer programming) | |
| dc.subject | Range (aeronautics) | |
| dc.subject | Fuel efficiency | |
| dc.subject | Aerodynamics | |
| dc.subject | Turbojet | |
| dc.subject | Altitude (triangle) | |
| dc.subject | Wing | |
| dc.subject | Aircraft flight mechanics | |
| dc.subject | Control theory (sociology) | |
| dc.subject | Physics | |
| dc.subject | Computer science | |
| dc.subject | Engineering | |
| dc.subject | Mathematics | |
| dc.subject | Geometry | |
| dc.subject.sdg | 7 | |
| dc.title | Approximate solutions of range for constant altitude – constant high subsonic speed flight of transport aircraft | |
| dc.type | Article | |
| dspace.entity.type | Publication | |
| local.authorid.openalex | A5023712238 | |
| local.authorid.openalex | A5082535208 |
