共 50 条
- [21] OPTIMUM SELECTION OF MAIN PARAMETERS FOR THE REVERSE DESIGN OF A SUPERSONIC MILITARY AIRCRAFT CANADIAN AERONAUTICS AND SPACE JOURNAL, 1980, 26 (03): : 218 - 229
- [22] Impact of aerodynamic modeling on control system design for a military aircraft concept AIAA AVIATION FORUM AND ASCEND 2024, 2024,
- [23] Military aircraft durability design method based on detail fatigue rating Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2010, 31 (12): : 2357 - 2364
- [25] To the theory of anticorrosion alloying of brasses PROTECTION OF METALS, 2005, 41 (02): : 138 - 145
- [26] A conceptual design methodology for predicting bleed and horsepower requirements of military aircraft engines JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1996, 118 (03): : 481 - 485
- [27] CCVS ACTIVE CONTROL TECHNOLOGY CREATING NEW MILITARY AIRCRAFT DESIGN POTENTIAL ASTRONAUTICS & AERONAUTICS, 1977, 15 (02): : 42 - 51
- [28] Night Vision Imaging Systems Design, Integration and Verification in Military Fighter Aircraft OPTICAL SENSING AND DETECTION II, 2012, 8439
- [30] Military aircraft camouflage coating AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2007, 79 (04): : 442 - 442