W.P. Henderson, and J.K. Huffman, Aerodynamic characteristic of a tandem wing configuration at a mach number of 0.30.Report X-72779, NASA, March 1975.,
V.S. Eger, Light duty box-wing aeroplane. U.S. Patent 5,503,352, April 2, 1996.,
R. Carlos, “Aircraft having a lambda-box wing configuration”.U.S. Patent 20110180660 A1, July 28, 2011.,
J. Wolkovitch, “Joined wing aircraft”.U.S. Patent 4,365,773, December 28, 1982.,
L. Miranda, “Boxplane wing and aircraft”. U.S. Patent 3,834,654,September 10, 1973,
A. Hernadi, “Method for improvement of the box wing aircraft
concept and corresponding aircraft configuration”.WIPO Patent
Cooperation Treaty 2016048211 A1, March 31, 2016,
L. Prandtl, “Induced drag of Multiplanes”.Technische Berichte,
Vol. III, No. 7, 1924,
A, Frediani, “The Prandtlwing, Lecture series on innovative configurations and advanced concepts for future civil aircraft”, Von
Karman Institute, VKI 2005-06, 2005.,
K. Balaji, S. Rathnavel, J. Vinoth, and V. Siva, "Experimental investigation of conceptual box wing aircraft", Int. J. Res. Aero Mech. Eng., vol. 4, no. 4, pp. 76-84, April 2016.
H. Smith, and P. Jemitola, A - 9 Box Wing Medium Range Airliner - Project Specification., Department of Aerospace Engineering, Cranfield University: Cranfield, 2009.
P.O. Jemitola, Conceptual Design and Optimization Methodology for Box Wing Aircraft., Department of Aerospace Engineering, Cranfield University: Cranfield, 2012.
D. Howe, Aircraft Loading and Structural Layout., Professional Engineering Publishing Limited: London, 2004.
L. Jenkinson, D. Rhodes, and P. Simpkin, Civil Jet Aircraft Design., Arnold Publishers: UK, 1999.
S.F. Hoerner, Fluid Dynamic Drag: Practical Information on Aerodynamic Drag and Hydrodynamic Resistance., Hoerner Fluid Dynamics: New Jersey, USA, 1965.
J. Roskam, Preliminary Calculation of Aerodynamic., Thrust and Power Characteristics, Roskam Aviation and Engineering Corporation: Kansas, USA, 1990.
J. Roskam, Airplane Cost Estimation: Design, Development., Manufacturing and Operating, Roskam Aviation and Engineering Corporation: Kansas, USA, 1990.
B. Pamadi, Performance, Stability, Dynamics and Control of Airplance., 2nd ed AIAA: Virginia, USA, 2004.