Add to ORKGA long range Mach 2.7 supersonic transport configuration concept was studied utilizing linear theory methods. The configuration was sized to carry 290 passengers 6,000 nautical miles nonstop. The final configuration has a maximum takeoff gross weight of 687,200 pounds, a wing loading of 69.8 lbf/sq.ft. and a thrust weight ratio of .278. The most significant result is that a significantly improved trimmed maximum lift drag ratio of 11.04 can be obtained for a supersonic transport at Mach 2.62 and 55,000 feet
Technical progress made in each of the disciplinary research areas affecting the design of supersoni...
An investigation was made in the Langley Unitary Plan wind tunnel at Mach numbers of 2.30, 2.96, and...
Research and development programs provide confidence that technology is in-hand to design an economi...
A systems study was conducted on an aircraft concept, representative of a supersonic-cruise military...
An analytical study of a supersonic-cruise, executive, jet aircraft indicated the effects of using a...
The design and analysis of a supersonic transport configuration was conducted using linear theory me...
This year, the senior level Aerospace Design class at Case Western Reserve University developed a co...
The impact of advanced supersonic technologies on the performance and characteristics of a supersoni...
A brief discussion is given of some recent experimental results obtained on a supersonic transport-t...
The impact of variable sweep wing technology with relaxed static stability requirements on a superso...
The results of the investigation showed that the configuration exhibits a sufficiently high drag div...
The results of four years research on technology are synthesized in an advanced supersonic cruise ai...
The applicability of sonic boom minimization concepts in the design of large supersonic transport ai...
A study was conducted to configure and analyze a 250 passenger, Mach 4 High Speed Civil Transport wi...
The relatively low values of lift-curve slope produced by highly swept arrow wings, coupled with the...
Technical progress made in each of the disciplinary research areas affecting the design of supersoni...
An investigation was made in the Langley Unitary Plan wind tunnel at Mach numbers of 2.30, 2.96, and...
Research and development programs provide confidence that technology is in-hand to design an economi...
A systems study was conducted on an aircraft concept, representative of a supersonic-cruise military...
An analytical study of a supersonic-cruise, executive, jet aircraft indicated the effects of using a...
The design and analysis of a supersonic transport configuration was conducted using linear theory me...
This year, the senior level Aerospace Design class at Case Western Reserve University developed a co...
The impact of advanced supersonic technologies on the performance and characteristics of a supersoni...
A brief discussion is given of some recent experimental results obtained on a supersonic transport-t...
The impact of variable sweep wing technology with relaxed static stability requirements on a superso...
The results of the investigation showed that the configuration exhibits a sufficiently high drag div...
The results of four years research on technology are synthesized in an advanced supersonic cruise ai...
The applicability of sonic boom minimization concepts in the design of large supersonic transport ai...
A study was conducted to configure and analyze a 250 passenger, Mach 4 High Speed Civil Transport wi...
The relatively low values of lift-curve slope produced by highly swept arrow wings, coupled with the...
Technical progress made in each of the disciplinary research areas affecting the design of supersoni...
An investigation was made in the Langley Unitary Plan wind tunnel at Mach numbers of 2.30, 2.96, and...
Research and development programs provide confidence that technology is in-hand to design an economi...