A study was conducted to determine whether subsonic manned research aircraft utilizing strut-braced wings of high-aspect-ratio had performance improvements when compared to a baseline concept. The effect of increased wing aspect ratio on structural weight, system weight, and maximum range and altitude was determined for configurations with and without strut bracing.
The significant results of the study indicated that an optimum cantilever configuration with a wing aspect ratio of 26 has a 19 percent improvement in cruise range when compared to a baseline concept with a wing aspect ratio ofapproximately 10. An optimum strut-braced configuration with a wing aspect ratio of 28 has a 31 percent improvement in cruise range when compared to the same baseline concept. The increased improvement in range capability is due to the reduction in wing weight resulting from the use of long, braced struts and the aerodynamic advantages in making these lifting struts. All configurations assume the same mission payload and fuel.