Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system - Info and Reading Options

By J. R. DeBonis

“Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system” Metadata:

Title: ➤ Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
Author: J. R. DeBonis

“Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system” Subjects and Themes:

Subjects: ➤ Computational fluid dynamics - Air breathing boosters - Pressure distribution - Propulsion - Wind tunnel tests - Hypersonic speed

Edition Identifiers:

The Open Library ID: OL11602711W

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