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CONSIDERATIONS OF LIFT ENGINE INSTALLATIONS IN VTOL AIRCRAFT FROM THE VIEWPOINT OF THE AIRFRAME DESIGNER
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Abstract
This paper outlines and discusses several of the important problems which must he solved by the airframe propulsion designer to obtain a high thrust-to-weight ratio lift engine installation. Problems considered include starting, air induction, exhaust, fire protection, and VTO control. The thrust-to-weight ratio degradation from bare engine to final installation is shwon for a typical example. Some installation requirements, which must also be considered by the engine designer, are noted.
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Citation
BAGBY, C., "CONSIDERATIONS OF LIFT ENGINE INSTALLATIONS IN VTOL AIRCRAFT FROM THE VIEWPOINT OF THE AIRFRAME DESIGNER," SAE Technical Paper 630074, 1963, https://doi.org/10.4271/630074.Data Sets - Support Documents
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