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Volrath Holmboe

  • Approximate theoretical pressure distribution due to lift and uniform pitch and roll for double-delta wings with subsonic leading edges at supersonic speedsApproximate theoretical pressure distribution due to lift and uniform pitch and roll for double-delta wings with subsonic leading edges at supersonic speeds
  • Charts for the position of the aerodynamic center at low speeds and small angles of attack for a large family of tapered wingsCharts for the position of the aerodynamic center at low speeds and small angles of attack for a large family of tapered wings
  • The center of pressure position at low speeds and small angles of attack for a certain type of delta wingThe center of pressure position at low speeds and small angles of attack for a certain type of delta wing