New PDF release: A simplified method for estimating the take-off weight for

By M. Arjomandi, N. K. Liseytsev

Airplane layout three (2000) forty nine - fifty six

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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. [26] Pessin DN. Aerodynamic analysis of hypersonic waverider aircraft. Master’s Thesis, California Polytechnic State University, San Luis Obispo, San Luis Obispo, CA, March 1993. [27] Johnson LM. Hydrodynamic flowfield visualization studies of a Mach 6 waverider. Master’s Thesis, Naval Postgraduate School, Monterey, CA, March, 1994. [28] 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. [25]. 9. Future design/research efforts Additional graduate student classroom design teams are expected to pursue the development of long-range tactical waverider configured aircraft.

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A simplified method for estimating the take-off weight for short-haul transports by M. Arjomandi, N. K. Liseytsev

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