Spillage-Adaptive Fixed-Geometry Bump Inlet of Wide Speed Range
In this work, a new spillage-adaptive bump inlet concept is proposed to widen the speed range for hypersonic air-breathing flight vehicles. Various approaches to improve the inlet start-ability are summarized and compared, among which the bump-inlet pattern holds the merits of high lift-to-drag rati...
Main Authors: | Zonghan Yu, Guoping Huang, Ruilin Wang, Omer Musa |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2021-11-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/8/11/340 |
Similar Items
-
Effects of Flow Spillage Strategies on the Aerodynamic Characteristics of Diverterless Hypersonic Inlets
by: Zonghan Yu, et al.
Published: (2022-11-01) -
Estimation Method and Verification of Pressure in Supersonic Inlet
by: LI Qiang, et al.
Published: (2020-12-01) -
Chesterfield Inlet (Canada) [peta]
Published: (1971) -
Research on Aerodynamic Layout of Three-Dimensional Inward Rotating Inlet Hypersonic Missile
by: Yang Huilin, Li Yiqing, Liu Tao, Zhang Hui, Tu Lianghui
Published: (2022-02-01) -
Clinical Characteristics of the Cervical Inlet Patch: A Case Series
by: Julian S. De La Chapa, et al.
Published: (2023-01-01)