Performance or Experimental channeled-Wall Annular Turbojet Combustor at Conditions Simulating high-Altitude Supersonic Flight; I - U-Shaped Channel Walls for Secondary-Air Entry: NACA Research Memorandum NO. E54L21a

Zettle, Eugene & Friedman, Robert

Edité par National Advisory Committee for Aeronautics, Wash. D.C., 1955

A propos de cet article

20pp. Previous owners rubber stamp on cover -associated. Marked declassified on cover. Probably printed in 1959. Charts, Diagrams, illustrations, etc. All of the librarian file cards - 8 exact duplicates still intact. Lewis Flight Propulsion Laboratory, Cleveland, Ohio. Size: 4to - over 9¾" - 12" tall.

N° de réf. du vendeur 005382

Détails bibliographiques

• Titre: Performance or Experimental channeled-Wall Annular Turbojet Combustor at Conditions Simulating high-Altitude Supersonic Flight; I - U-Shaped Channel Walls for Secondary-Air Entry: NACA Research Memorandum NO. E54L21a
• Éditeur: National Advisory Committee for Aeronautics, Wash. D.C.
• Date de parution: 1955
• Reliure: Decor/Stiff Blue Card Stock
• Édition: Original Edition.
• État de l'article: VG+