Geoffrey Terence Roland Hill, (1895 – 26 December 1955) was a British aviator and aeronautical engineer. Early life Geoffrey Terence Roland Hill was born in 1895, the son of Michael J. M. Hill, Professor of Mathematics at the University College London, and his wife Minnie. He was educated at University College School. While he was in his early teens he won prizes as a builder of model aircraft. In 1912, with his younger brother, Roderic, they built a model aircraft for the Children's Exhibition at Olympia, which was followed by a nearly-successful full-sized glider. Subsequently, he went up to University College, where he obtained a Bachelor of Science in 1914 and joined the Royal Aircraft Factory as a graduate apprentice. Flying career By 1916 Hill had learnt to fly and became a test pilot at the Royal Aircraft Factory. He obtained a commission in the Royal Flying Corps as 2nd lieutenant, and fought in France with No. 29 Squadron. In late 1916 he was awarded the Military Cross and in January 1917 he was promoted to the rank of captain (temporary). Invalided home, he moved back into test flying and by 1918 he was in command of the Aerodynamics Flight at the Royal Aircraft Establishment. When the war ended he joined Handley Page, Ltd., as their chief test pilot/aerodynamicist, and in 1919 climbed a Handley page W.8 up to nearly 14,000 ft – then, a world record for an aircraft of 1,500 kg all-up weight Aeronautics Hill designed a series of tailless aircraft, the Westland-Hill Pterodactyls, from the 1920s onwards. After the last Pterodactyl flew in 1932, he ended his association with Westland Aircraft in order to take up a chair as Professor of Engineering Science at London University. In 1939 he headed a project in Pawlett, near Bridgwater, Somerset, investigating methods for cutting the cables on enemy barrage balloons; recovery from stalling after contact with such cables was an important part of his work there. Hill was British Scientific Liaison Officer at the National Research Council (NRC) in Canada in the mid-1940s. There, he made the proposal for the NRC tailless glider for the study of the control and stability of tailless aircraft. The glider design was built and flew from 1946 until the project ended around 1950. Hill proposed the "aero-isoclinic" wing in 1951, in an attempt to control the undesirable effects of bending in the long, thin