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- Busemann進(jìn)氣道Busemann inlet
- 為了研究流線(xiàn)追蹤Busemann進(jìn)氣道在低馬赫數來(lái)流條件下的起動(dòng)性能、總體性能以及抗反壓能力,對設計馬赫數5.3、收縮比CR=5的6°截短后的流線(xiàn)追蹤進(jìn)氣道進(jìn)行了馬赫數3.85風(fēng)洞實(shí)驗.A wind-tunnel testing of a streamline traced hypersonic Busemann inlet,with a designed Mach 5.3 and shrinkage ratio CR=5,was conducted at Mach 3.85 to study its starting and overall performance as well as back-pressure capability below Mach 5.3 conditions.
- Busemann不等式Busemann s inequality
- Busemann-Petty問(wèn)題Busemann-Petty problem
- 進(jìn)氣道inlet channel
- 超音速進(jìn)氣道supersonic inlet
- 二元進(jìn)氣道two dimensional inlet
- 外掛進(jìn)氣道external stores inlet
- 具有導氣屏結構的內燃機進(jìn)氣道流場(chǎng)的三維數值模擬研究The Study of Three-Dimensional Flow in Intake Duct With Gas Leading Screen in Internal Combustion Engine
- 帶進(jìn)氣道With inlets
- 主進(jìn)氣道main air intake
- 雙進(jìn)氣道twin inlet
- 雙S進(jìn)氣道line-of-sight blockage
- S形進(jìn)氣道S-duct inlet
- S彎進(jìn)氣道S-shaped inlet
- 一種背負式無(wú)附面層隔道進(jìn)氣道的數值模擬研究與實(shí)驗驗證Numerical Simulation Investigation and Experimental Validation of a Top-mounted Diverterless Inlet and Its Validation
- 切向進(jìn)氣道進(jìn)氣tangential duct intake
- 翼根進(jìn)氣道wing-root inlet
- 錐形進(jìn)氣道conical inlet
- 凸包進(jìn)氣道bump inlet
