keysersoze
New Member
This may have been covered before so forgive me if I am covering old ground. According to the info-page on the J-7 it claims that...
"This design offered an excellent solution to the inherent low aspect ratio problem of a slender delta. The slighting larger wingspan and 8.17% more wing area also gave an increased internal fuel capacity (from 2,080kg to 4,165kg) and much enhanced manoeuvrability."
Now someone has asked me how is it possible for 8.17% wing area to translate into double the fuel capacity? Or is the data incorrect?
"This design offered an excellent solution to the inherent low aspect ratio problem of a slender delta. The slighting larger wingspan and 8.17% more wing area also gave an increased internal fuel capacity (from 2,080kg to 4,165kg) and much enhanced manoeuvrability."
Now someone has asked me how is it possible for 8.17% wing area to translate into double the fuel capacity? Or is the data incorrect?