EFFECT OF LEADING-EDGE SEPARATION ON THE LIFT OF A DELTA-WING

[1] LEADING-EDGE SEPARATION FROM DELTA-WINGS AT SUPERSONIC SPEEDS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (06): : 430 - 430

[2] ANTON L, 1939, INGENIEUR ARCH DEZ

[3] JONES RT, 1946, NACA TR835

[4] Kaden H., 1931, ING ARCH, V2, P140, DOI 10.1007/BF02079924

[5] KIRCHHOFF G, 1869, CRELLE J MATH, V70, P289

[6] LEGENDRE R, 1953, RECHERCHE AERONAUTIQ

[7] LEGENDRE R, 1952, RECHERCHE AERONAUTIQ

[8] MUNK M, 1924, NACA TR184

[9] PRANDTL L, 1922, HYDRO AERODYNAMIK

[10] von Karman T, 1912, PHYS Z, V13, P49

[1] LEADING-EDGE SEPARATION FROM DELTA-WINGS AT SUPERSONIC SPEEDS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (06): : 430 - 430

[2] ANTON L, 1939, INGENIEUR ARCH DEZ

[3] JONES RT, 1946, NACA TR835

[4] Kaden H., 1931, ING ARCH, V2, P140, DOI 10.1007/BF02079924

[5] KIRCHHOFF G, 1869, CRELLE J MATH, V70, P289

[6] LEGENDRE R, 1953, RECHERCHE AERONAUTIQ

[7] LEGENDRE R, 1952, RECHERCHE AERONAUTIQ

[8] MUNK M, 1924, NACA TR184

[9] PRANDTL L, 1922, HYDRO AERODYNAMIK

[10] von Karman T, 1912, PHYS Z, V13, P49