By M. Arjomandi, N. K. Liseytsev
Airplane layout three (2000) forty nine - fifty six
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Additional resources for A simplified method for estimating the take-off weight for short-haul transports
Several graduate students may soon combine their individual thesis research efforts to develop a more detailed tactical carriercapable waverider-configured aircraft design than is currently possible with the classroom design teams. 10. Conclusions 1. 34M 45 with corresponding combat radii in the neighborhood of 580 nm4R41500 nm. F. Newberry / Aircraft Design 1 (1998) 159—191 2. Weight limitations in the neighborhood of 80,000 lbf do not appear to be a constraint for the development of carrier-capable waverider-configured aircraft.
Preprint AIAA-95-0849, 33rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 9—12 January, 1995.  Pessin DN. Aerodynamic analysis of hypersonic waverider aircraft. Master’s Thesis, California Polytechnic State University, San Luis Obispo, San Luis Obispo, CA, March 1993.  Johnson LM. Hydrodynamic flowfield visualization studies of a Mach 6 waverider. Master’s Thesis, Naval Postgraduate School, Monterey, CA, March, 1994.  Cedrun ME. Low-speed wind tunnel testing of the NPS/NASA Ames Mach 6 optimized waverider.
3;10. Fig. 27. 3;10. F. Newberry / Aircraft Design 1 (1998) 159—191 189 Fig. 28. 3;10. Vanhoy waverider did not have an integrated airframe/engine installation whereas the Price model did possess an engine installation (although there was no flow through the core area). A more complete discussion of the Price waverider has been presented by Newberry et al. . 9. Future design/research efforts Additional graduate student classroom design teams are expected to pursue the development of long-range tactical waverider configured aircraft.
A simplified method for estimating the take-off weight for short-haul transports by M. Arjomandi, N. K. Liseytsev