Correlated optimum lift coefficient and thrust-vector angle for longitudinal performance-Reference-Cited by-同舟云学术

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Correlated optimum lift coefficient and thrust-vector angle for longitudinal performance

Published:2017-08 Issue: Volume:67 Page:141-143
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Bovet Laurent

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference5 articles.

1. G. Gilyard, A. Bolonkin, Optimal Pitch Thrust-Vector and Benefits for all Flight Regimes, NASA/TM-2000-209021.

2. Aerodynamics, Aeronautics, and Flight Mechanics;McCormick,1995

3. Aircraft Engine Design;Mattingly,2002

4. Flight Dynamics;Stengel,2004

5. Avions civils à réaction: Plan 3 vues et données caractéristiques;Roux,2007

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical simulation and experiment of a bypass dual throat nozzle with tab modification;Aerospace Science and Technology;2024-01

2. Exploring Hysteresis Phenomena in the Shock-Induced Thrust Vector Nozzle;2024

3. Experimental Study of the Vector Nozzle Performance Using Calibration Tank;Lecture Notes in Electrical Engineering;2019

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