Flight Investigation of an Underwing Nacelle Installation of Three Variable-flap Ejector Nozzles
Author : Verlon L. Head
Publisher :
Page : 52 pages
File Size : 35,42 MB
Release : 1972
Category : Airplanes
ISBN :
Scientific and Technical Aerospace Reports
Author :
Publisher :
Page : 978 pages
File Size : 38,66 MB
Release : 1976
Category : Aeronautics
ISBN :
Book Description
NASA Reference Publication
Author :
Publisher :
Page : 116 pages
File Size : 18,42 MB
Release : 1977
Category : Astronautics
ISBN :
Book Description
Flight Investigation of Installation Effects on a Plug Nozzle with a Series of Boattailed Primary Shrouds Installed on an Underwing Nacelle
Author : Verlon L. Head
Publisher :
Page : 36 pages
File Size : 27,65 MB
Release : 1974
Category : Airplanes
ISBN :
Book Description
NASA Technical Memorandum
Author :
Publisher :
Page : 438 pages
File Size : 16,78 MB
Release : 1974
Category : Aeronautics
ISBN :
Book Description
NASA Technical Note
Author :
Publisher :
Page : 620 pages
File Size : 20,15 MB
Release : 1973
Category :
ISBN :
Book Description
Flight Investigation of Airframe Installation Effects on a Variable Flap Ejector Nozzle of an Underwing Engine Nacelle at Mach Numbers from 0.5 to 1.3
Author :
Publisher :
Page : 126 pages
File Size : 17,66 MB
Release : 1970
Category :
ISBN :
Book Description
Comparison of Ground and Flight Test Results Using a Modified F106B Aircraft
Author :
Publisher :
Page : 42 pages
File Size : 44,1 MB
Release : 1973
Category :
ISBN :
Book Description
Flight and Wind Tunnel Investigation of Installation Effects on Underwing Supersonic Cruise Exhaust Nozzles at Transonic Speeds
Author :
Publisher :
Page : 28 pages
File Size : 25,86 MB
Release : 1970
Category :
ISBN :
Book Description
Aeronautical Engineering
Author :
Publisher :
Page : 580 pages
File Size : 10,63 MB
Release : 1971
Category : Aeronautics
ISBN :
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
