1 |
Munk, M.M., General Biplane Theory, National Advisory Committee for Aeronautics. Washington, DC, United States, 1922.
|
2 |
Norton, F.H., "The Effects of Staggering a Biplane", NACA TN 70., 1921.
|
3 |
Mock, R.M., The Distribution of Loads Between the Wings of a Biplane having Decalage, in NACA TN 269. 1927.
|
4 |
Knight, M., and R.W. Noyes, Wind Tunnel Pressure Distribution Tests on a Series of Biplane Wing Models Part I. Effects of Changes in Stagger and Gap, in NACA TN 310. 1929.
|
5 |
Traub, L.W., "Theoretical and Experimental Investigation of Biplane Delta Wings",. Journal of Aircraft, Vol 38, No. 3, 2001, pp. 536-546.
DOI
ScienceOn
|
6 |
Polhamus, E.C., A Concept of the Vortex Lift of Sharp-Edge Delta Wings Based on a Leading-Edge-Suction Analogy, in NASA Technical Note. 1966: Washington, D.C.
|
7 |
Moschetta, J.-M. and C. Thipyopas, Aerodynamic Performance of a Biplane Micro Air Vehicle. Journal of Aircraft, 2007. 44(1): p. 291-299.
DOI
ScienceOn
|
8 |
Barlow, J.B., W.H. Rae, and A. Pope, Low-Speed Wind Tunnel Testing. 2nd ed. 1999.
|
9 |
Grasmeyer, J.M., and M.T. Keennon, "Development of Black Widow Micro Air Vehicle", 39th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, 2001.
|