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Conceptual redesign of the B-1B bomber inlets for improved supersonic performance

  • Published:2015-09 Issue: Volume:45 Page:476-483
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Berra Lee M.,Slater John W.,Olcmen Semih M.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference12 articles.

1. Intake Aerodynamics;Seddon,1985

2. A performance study of a super-cruise engine with isothermal combustion inside the turbine;Ya-tien,2004

3. Design and analysis tool for external-compression supersonic inlets;Slater,2012

4. Aircraft Propulsion;Farokhi,2008

5. Some design considerations for supersonic cruise mixed compression inlets;Bowditch,1973

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1. A Study on Design of S-Duct Structures and Air Intake for Small Aircraft Applied to High Strength Carbon–Epoxy Composite Materials;Materials;2022-04-20

2. Aerodynamic design and evaluation of an open-nose supersonic drone;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-04-15

3. The inlet flow structure of a conceptual open-nose supersonic drone;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-02-25

4. Flow Field Study of Mixed Compression Supersonic Air Intake with Cowl Ventilation;Journal of Applied Fluid Mechanics;2020-11-01

5. Optimum design of the inlet port profile of a ramjet extended range projectile;Journal of Physics: Conference Series;2020-03-01
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