Engineering Design Handbook - Elements of Aircraft and by ARMY MATERIEL COMMAND ALEXANDRIA VA

By ARMY MATERIEL COMMAND ALEXANDRIA VA

This 1969 guide replaces AMCP 706-282, Propulsion and Propellants guide and isn't in basic terms a revision to replace the textual content fabric. This instruction manual is meant to supply engineers and army team of workers with a common description of the features and layout positive factors of the propulsion platforms for missiles and airplane both hired in or being built for weapon platforms. The guide is split into components: half One: Chemical Rocket Propulsion and half : Air-breathing Jet Propulsion Engines. half represents the hot addition that is dedicated to air-breathing engines, except piston engines, hired for propelling winged plane, helicopters, and goal drones.

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Charts Presenting Relationships Between the Parameters for Oblique Shocks . . . . . . . 5 A-1 1 A-12 A-13 Page Application of Normal Shock Table to Oblique A-93 Shocks . . . . . . . . . . . . . . . . Supersonic Flow Over an Infinite Wedge . . . . . . . . A-94 Supersonic Flow Over a Cone ....................... A-98 Prandtl-Meyer Expansion Flow ..................... A-99 References . . . . . . . . . . . . . . . . . . . A- 112 . APPENDIX B USEFUL TABLES.

5 xx Page Critical Static Temperature (T*) . . . . . . . Critical Expansion Ratio (P*/Po) . . . . . . Critical Density Ratio @ * / P O ) . . . . . . . Dimensionless Velocity (M* = u/a*) . . . . . Relationships Between the Reference Speeds ao andc, ................................... 40 ......................... Energy Equations in Terms of the Reference SpeedsaO and co ....................... Critical Area Ratio for the Steady Onedimensional Isentropic Flow of an Ideal Gas .

Adiabatic Flow With Wall Friction in a Constant Area Duct . . . . . . . . . . . . . . . . . Friction Coefficient (f) . . . . . . . . . . Friction Coefficient for Compressible and Incompressible Flows . . . . . . . . . . Fanno Line Equation for Steady Adiabatic Flow in a Constant Area Duct . . . . . . . . . . . . Fanno Line Equation for the Flow of an Ideal Gas in a Constant Area Duct . . . . . . . . . . . Friction Parameter for a Fanno Flow .

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