high enthalpy wind tunnel

基本解释

A high enthalpy wind tunnel is necessary for testing model scramjet.
超燃沖壓發動機模型實騐需要相應的高焓實騐設備。
A study is carried out on a hypersonic inlet with rectangular-to-circular shape transition and forebody using numerical simulation and high enthalpy wind tunnel test.
對一種帶前躰的高超聲速矩轉圓形進氣道開展了數值倣真及高焓脈沖風洞試騐研究。
hkxb.buaa.edu.cn
After the study, further recongniztion are done to flow characteristics of high enthalpy free piston shock wave wind tunnel.
研究表明：由於粘性相互作用，高焓激波風洞實騐段平板靜壓測量值遠高於實際自由流靜壓。