Effect of Fuselage Cross Section on Aerodynamic Characteristics of Reusable Launch Vehicles

Open Journal of Fluid Dynamics
doi 10.4236/ojfd.2016.63017
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Scientific Research Publishing, Inc.

Related search

Effect of Ground Proximity on Aerodynamic Forces and Moments of Reusable Launch Vehicle at Subsonic Speed

International Journal of Research in Engineering and Technology
2016English

Structural Concepts and Aerodynamic Analysis for Low Radar Cross Section (LRCS) Fuselage Configurations

1978English

Mid-Air Retrieval Technology for Returning of Reusable Launch Vehicles' Boosters

2009English

Pre-Launch Diagnostics for Launch Vehicles

IEEE Aerospace Conference Proceedings
SpacePlanetary ScienceAerospace Engineering
2008English

Concept Study of a Reusable Suborbital Launch Vehicle

2018English

Review on Aerodynamic Drag Reduction of Vehicles

International Journal of Engineering Materials and Manufacture
2019English

Wake Dynamics and Rotor-Fuselage Aerodynamic Interactions

Journal of the American Helicopter Society
2009English

Dynamics Sensor Validation for Reusable Launch Vehicle Propulsion

1998English

Effect of Cross Section of Spandex Yarn on Air Drag.

Sen'i Kikai Gakkaishi (Journal of the Textile Machinery Society of Japan)
1997English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy