SAWE Report - Cal Poly San Luis Obispo

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17. NACA-TN-3182, “Manual of the ICAO Standard Atmosphere <strong>Cal</strong>culations by the NACA”, NASA, 1976 18. Nicolai, L. M. Fundamentals of Aircraft Design, METS Inc., <strong>Cal</strong>ifornia, 1984. 19. Oates, G. C. Aircraft Propulsion Systems Technology and Design, AIAA, Washington DC, 1989. 20. Raymer, D. P. Aircraft Design: A Conceptual Approach – Third Edition, AIAA, Washington DC, 1999. 21. Roskam, J. Airplane Design, Part I: Preliminary Sizing of Airplanes, DARcorporation, Kansas, 1997. 22. Roskam, J. Airplane Design, Part II: Preliminary Preliminary Configuration Design and Integration of the Propulsion System, DARcorporation, Kansas, 1997. 23. Roskam, J. Airplane Design: Part III, Roskam Aviation And Engineering Corporation, Ottawa, KS, 1989, pp 1-34. 24. Roskam, J. Airplane Flight Dynamics and Automatic Flight Controls, DARcorporation, Kansas, 1979. 25. Wilcox, F. J., Baysal, O., Stallings, R. L., “Tangential, Semisubmerged, and Internal Store Carriage and Separation,” Tactical Missile Aerodynamics: General Topics, Edited by Michael J. Hemsch, Vol. 141, Progress in Aeronautics and Astronautics, AIAA, New York, 1992, pp. 667-721. 26. www.aeronautics.ru/nws002/f22/diagram05.jpg 27. www.aeronautics.ru/nws002/f22/diagram06.jpg 28. www.aeronautics.ru/nws002/f22/systems.htm 29. www.af.mil/news/efreedom/bombs.html 30. www.af.mil/news/factsheets/KC_10A_Extender.html 31. www.af.mil/news/factsheets/KC_135_stratotanker.html 32. www.arfl.afr.mil 33. www.aoe.vt.edu/aoe/faculty/Mason_f/M96SC.html 34. www.batnet.com/mfwright/spacesuit.html 108
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SAWE Paper No. 3232 Category No. 10
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Table of Contents Abstract_________
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List of Figures Figure 1.1 - Design
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Figure 13.4 - Rectilinear Vision Pl
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Nomenclature AIAA American Institut
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α Angle of Attack, degrees, rad.
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Table 1.II - Summary of Design Requ
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Figure 1.3 - F-15 Strike Eagle F-11
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Table 1.III - Comparison of the F-1
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Many of the equations buried in the
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3 Configuration The current configu
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Another problem arises from the 20
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• Span = 54.7 ft • m.a.c. = 32
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4 Stealth Considerations As mention
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Table 4.I - Common Ground Radars Ra
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30 20 10 0 -10 -20 -30 -40 -50 1 GH
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5 Aerodynamics The major aerodynami
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1 GHz. 40º LE Sweep 10 GHz. 40º L
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5.3 Wing Thickness The effect of wi
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5.4 Airfoil The NACA 65A-003 airfoi
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1 Section Lift Coefficient 0.9 0.8
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90 80 Wing Cross Sectional Area (ft
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6 Propulsion In developing the prop
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Table 6.II - RFP Dimensions Compare
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38 Figure 6.1 - VAATE Goals
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TSFC 3.0 2.8 2.6 2.4 2.2 2.0 1.8 1.
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Deflection Angle Analysis for Mach
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Figure 6.8 - Cost Association with
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The inlet has a boundary layer dive
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7 Materials and Structure The overa
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Vertical Attachment Points Horizont
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8 Landing Gear Landing Gear design
Page 65 and 66: steel. This means that more braking
Page 67 and 68: Table 9.II - Final Component Weight
Page 69 and 70: throughout the 5-hour mission. Usin
Page 71 and 72: 10 Stability and Control To initial
Page 73 and 74: difference in neutral point and cen
Page 75 and 76: 40 30 20 10 0 -10 -20 -30 -40 -50 2
Page 77 and 78: The Vendetta configuration utilizes
Page 79 and 80: -0.6 -0.4 UNSTABLE NEUTRAL -0.2 Lif
Page 81 and 82: Validation of an aircraft design su
Page 83 and 84: consumption. The main aspects of th
Page 85 and 86: In addition to the performance requ
Page 87 and 88: 70,000 Altitude (ft) 60,000 50,000
Page 89 and 90: 11.4 Mission Requirements By comple
Page 91 and 92: Table 11.VIII - Landing Flight Prof
Page 93 and 94: 11.7 Alternate Missions In addition
Page 95 and 96: 12 Payload Weapon internal layout d
Page 97 and 98: 13 Cockpit Cockpit Design began wit
Page 99 and 100: that could be used in landing and t
Page 101 and 102: 14 Systems The systems of the Vende
Page 103 and 104: 14.3 Fuel System Initial fuel syste
Page 105 and 106: 15 Manufacturing Several manufactur
Page 107 and 108: 16 Cost Analysis The final and perh
Page 109 and 110: Appendix Threats Chart Common Surfa
Page 111 and 112: Wing Break Point Fuel Aft Fuselage
Page 113 and 114: The Vendetta Design Team Chris Atki
Page 115: References 1. “Ejection Systems,
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SAWE Report - Cal Poly San Luis Obispo

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