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Flight and wind tunnel investigation of installation effects on underwing supersonic cruise exhaust nozzles at transonic speeds

Author
Blaha, B J.
Published
[Place of publication not identified] : [publisher not identified], 1970.
Physical Description
14 pages
Additional Creators
American Institute of Aeronautics and Astronautics. Technical Information Service

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Language Note
In English.
Subject(s)
Collection
IAA papers.
Note
Reproduced from: Flight And Wind Tunnel Investigation Of Installation Effects On Underwing Supersonic Cruise Exhaust Nozzles At Transonic Speeds (Airframe Installation Effects At Transonic Speeds On Underwing Supersonic Cruise Exhaust Nozzles, Using Flight And Wind Tunnel Tests)
Abstracted in International Aerospace Abstracts.
A70-43274.
Reproduction Note
Microform. New York : American Institute of Aeronautics and Astronautics, Technical Information Service, [19--?]
View MARC record | catkey: 19149278