Home › Aeronautics & Astronautics › Theory of Aerospace Propulsion

Theory of Aerospace Propulsion

by Pasquale M. Sforza

A foundation in aircraft-engine analysis and preliminary propulsion design

Regular price $143.49 USD
Regular price $143.49 USD Sale price $143.49 USD

Paperback New English

Delivery to your door
In stock·Dispatches in 1–2 business days
Standard shipping* from $4.35
Standard shipping transit* 5–8 business days after dispatch

Faster options are available.

Rates and delivery estimates depend on your destination and item quantity. Estimates are informational only; the final shipping method and rate are selected at checkout.

Secure checkout
American Express Apple Pay DiscoverGoogle Pay Mastercard PayPalVisa
30-day eligible returns Returns & refunds policy

AlbakiReads Editorial

A foundation in aircraft-engine analysis and preliminary propulsion design

Built around fluid mechanics and thermodynamics, this second edition connects core engineering principles to the analysis of aircraft engines and gas-turbine propulsion systems. It addresses how propulsion configurations are assessed for particular flight conditions, then extends that work into system studies and preliminary aerothermal design for turbomachinery components. The book also frames propulsion design as a comparative process, covering the conception, analysis, and optimization of alternatives for both conventional and unconventional missions. Revised content, examples, problems, and illustrations position it as a substantial instructional text for working through key aerospace-propulsion concepts.

Good fit for readers who enjoy

  • Engineering students studying aerospace propulsion
  • Learners applying thermodynamics and fluid mechanics to aircraft engines
  • Students working on preliminary turbomachinery or propulsion-system design

Themes

Aircraft enginesGas-turbine propulsionFluid mechanicsThermodynamicsTurbomachinery design

Based on publisher information and book metadata.

Book overview

Theory of Aerospace Propulsion, Second Edition, teaches engineering students how to utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems, be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions and preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. This updated edition has been fully revised, with new content, new examples and problems, and improved illustrations to better facilitate learning of key concepts.

Shipping & returnsShipping options, delivery timing, and our return policy.

In-stock items normally dispatch within 1–2 business days. The ZIP-code estimator on this page is informational only; the final shipping method, price, and availability are confirmed at checkout for your full order.

For the initial delivery estimate we use these transit windows after dispatch: Standard 5–8 business days, Expedited 2–4 business days, and Priority 1–2 business days. Holiday delays are not included.

Eligible items can be returned within 30 days in accordance with our return policy.

Customer reviews