The class of slender, axisymmetric missiles of given length, base radius, and specific weight is considered under the assumptions that the pressure distribution is modified Newtonian and the surface-averaged skin-friction coefficient is constant. The problem of minimizing the ballistic factor is formulated and solved via the calculus of variations for the case where the nose radius of the missile has a specified value, not necessarily zero
Raleigh-Ritz method has been applied to solve the problem of determining optimum blunt-nosed missil...
In the hypersonic regime, noncircular missiles have attracted significant attention from researchers...
Slender body methods have been applied to some specialized problems associated with missile configur...
The problem of determining the geometry of slender, axisymmetric missiles of minimum ballistic fact...
Minimum ballistic factor for slender axisymmetric power law bodies have been obtained by taking a va...
Abstract. The problem of determining the geometry of non-slender axisymmetric missile of minimum bal...
The problem of determining the geometry of non-slender axisymmetric missile of minimum ballistic fac...
The problem of finding geometries of minimum re-entry time missile has been reduced to a problem in ...
Raleigh-Ritz method has been applied to solve the problem of determining optimum blunt-nosed missil...
In the hypersonic regime, noncircular missiles have attracted significant attention from researchers...
Slender body methods have been applied to some specialized problems associated with missile configur...
The problem of determining the geometry of slender, axisymmetric missiles of minimum ballistic fact...
Minimum ballistic factor for slender axisymmetric power law bodies have been obtained by taking a va...
Abstract. The problem of determining the geometry of non-slender axisymmetric missile of minimum bal...
The problem of determining the geometry of non-slender axisymmetric missile of minimum ballistic fac...
The problem of finding geometries of minimum re-entry time missile has been reduced to a problem in ...
Raleigh-Ritz method has been applied to solve the problem of determining optimum blunt-nosed missil...
In the hypersonic regime, noncircular missiles have attracted significant attention from researchers...
Slender body methods have been applied to some specialized problems associated with missile configur...