distribution of pressure on slender wings with 'similar' cross-sections at zero lift in supersonic flow
By: J. H. Durran and W. T. Lord.
Contributors: Lord, W. T.; Royal Aircraft Establishment (Great Britain)
Series: Royal Aircraft Establishment. Technical note -- no. AERO.2591
Publisher: Royal Aircraft Establishment
Published: 1958
Place of publication: Farnborough, Hants
Number of pages: 17
Notes: Bibliographical references: p.11.