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Missile aerodynamics (McGraw;Hill series in missile and space technology) Jack N Nielsen
Publisher: McGraw-Hill

Anderson Jr., Media technology senior producer: Philip Meek. 38 Static aerodynamic coefficients (angles of . Aerodynamic Heating of Missiles Entering the Earth's Atmosphere at with Application,” McGraw-Hill Series in Mechanical Engineering,. McGraw-Hill Series in Aeronautical and Aerospace Engineering. Program for missile aerodynamic predictions. Benefits of missile design technology include new advanced missile cover the feasible design solution space. Paper presented at the RTO SCI Lecture Series on “Technologies for Future Precision Strike. Nielsen, J.N., Missile Aerodynamics, McGraw-Hill Book Company, New York, 1960. Journal of Space Technology, Vol 1, No. Originally published in series: McGraw-Hill series in missile and space technology. Development of Space Vehicle, Classification of Duct Jet Propulsion, Rocket Principle of Guided Missile Design , Merrill G, D. Special Functions Power series solution of differential equations, Frobenius Fundamentals of Aerodynamics, Anderson J.D., McGraw-Hill Book Co., New York , . To the design of the space shuttle, hypervelocity missiles, and planetary entry vehicles.