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Artificial Stability and Control of Longitudinal Motion of the F-94 Aircraft. Theoretical Investigation.


AD007115

Publication Date 1952
Personal Author HEILENDAY, F. W.
Page Count 10
Abstract No abstract available.
Keywords
  • Jet fighters
  • Control
  • Pitch (Motion)
  • Theory
Source Agency
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
Corporate Authors Cornell Aeronautical Lab., Inc., Buffalo, NY.
Supplemental Notes Report on Artificial Stability on Military Aircraft.
Document Type Technical Report
NTIS Issue Number 198107
Contract Number
  • AF33 038 20659
Artificial Stability and Control of Longitudinal Motion of the F-94 Aircraft. Theoretical Investigation.
Artificial Stability and Control of Longitudinal Motion of the F-94 Aircraft. Theoretical Investigation.
AD007115

  • Jet fighters
  • Control
  • Pitch (Motion)
  • Theory
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
  • AF33 038 20659
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