1162. Design Considerations in Formulating V/STOL Lift Plus Lift/Cruise Supersonic Fighter Concepts
$20.00
SAWE Members get a $200 store credit each year.*
*Store credit coupon available at checkout, click the button in your shopping cart to apply the coupon.
Not applicable to SAWE textbooks and current conference technical papers.
Paper
Abstract
Several means of providing V/STOL thrust are examined and discussed relative to their impact on the design of supersonic fighters. The lift plus lift/cruise concept is discussed in more detail, specifically addressing both the advantages and concerns that exist with that system. The principal concern is the operational footprint (temperature and noise). The principal advantage is its minimal impact on airframe design, aerodynamic parameters, and fuel requirements, which are the major parameters in weight growth spiral effects. The conclusion is that lift plus lift/cruise advances result from differences that are fundamental, and that this concept will generally result in the lightest weight and lowest cost supersonic fighter designed to a specific operational requirement.
