1

Hypersonic flow over a narrow delta plate at large angles of attack

Année:
1992
Langue:
english
Fichier:
PDF, 219 KB
english, 1992
2

The shapes of bodies with maximum lift-to-drag ratio in supersonic flow

Année:
2009
Langue:
english
Fichier:
PDF, 376 KB
english, 2009
3

Supersonic flow past circular cones at large angles of attack

Année:
1973
Langue:
english
Fichier:
PDF, 491 KB
english, 1973
8

Calculation of supersonic flow around v-shaped wings by the fitting method

Année:
1971
Langue:
english
Fichier:
PDF, 391 KB
english, 1971
9

Supersonic gas flow past the leeward side of a conical wing

Année:
1973
Langue:
english
Fichier:
PDF, 656 KB
english, 1973
10

Solution of the problem of the flow around a V-shaped wing with a strong shock at the leading edge

Année:
1973
Langue:
english
Fichier:
PDF, 447 KB
english, 1973
11

Normal force of a flat triangular wing in a supersonic flow

Année:
1977
Langue:
english
Fichier:
PDF, 151 KB
english, 1977
12

Investigation of supersonic three-dimensional flow past pointed axisymmetric bodies

Année:
1986
Langue:
english
Fichier:
PDF, 626 KB
english, 1986
14

Conical wing of maximum lift-drag ratio in a supersonic gas flow

Année:
1986
Langue:
english
Fichier:
PDF, 525 KB
english, 1986
15

Solution of the problems of spacecraft aerothermodynamics

Année:
2012
Langue:
english
Fichier:
PDF, 385 KB
english, 2012