Design of hypersonic aircraft
Design of hypersonic aircraft
- New search for: Multhopp, H.
- New search for: Multhopp, H.
Aircraft has to fit following flight regimes; orbital, hypersonic, supersonic transonic, and subsonic + landing; selection of right compromises between often contradictory conditions; problem of longitudinal stability; subsonic and hypersonic lift-drag ratio and aerodynamic heating are examined; it is shown that hypersonic lift drag ratio has to be determined by restraints which aerodynamic heating problem imposes on design.
Document information
Design of hypersonic aircraft
Aero/Space Eng
Aerospace Engineering ; 20 , n 2
1961
Article (Journal)
English
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