Discussion Overview
The discussion revolves around the feasibility of using a car engine to drive a handmade axial turbofan for thrust generation, exploring concepts related to power supply, turbine design, and performance metrics. Participants delve into the mechanics of airflow, torque, horsepower, and the implications of using exhaust gases in this context.
Discussion Character
- Exploratory
- Technical explanation
- Debate/contested
Main Points Raised
- One participant proposes using a 350 small block Chevy engine to drive a turbofan, aiming for high horsepower and torque to generate thrust.
- Another participant questions the clarity of terms such as "power supply" and "9 stage turbine," seeking clarification on whether it refers to multiple turbines or compression stages.
- Concerns are raised about the feasibility of hand-making turbines, which require precision engineering.
- Participants discuss the concept of running exhaust through the turbine, noting that this is a standard operation in jet engines.
- There is a debate about the implications of a 1:5 gear ratio, with some arguing that it could lead to mechanical failure while others suggest it could increase turbine speed.
- One participant expresses skepticism about achieving significant thrust without combustion, suggesting that compressing air without burning fuel may not yield the desired results.
- Another participant shares insights from a school discussion on torque versus horsepower, illustrating how different power characteristics affect vehicle performance.
- Clarifications are made regarding the intention to create a jet car that could operate at idle while still producing thrust.
Areas of Agreement / Disagreement
Participants express differing views on the feasibility and mechanics of the proposed system. There is no consensus on the effectiveness of using a car engine to drive a turbofan for thrust generation, and multiple competing perspectives on the design and operation remain unresolved.
Contextual Notes
Participants highlight limitations in understanding the precise mechanics of turbine operation, the implications of gear ratios, and the relationship between torque and horsepower in the context of thrust generation.