Thrust and wing loading requirements for short haul aircraft constrained by engine noise and field lenght/

Main Author: Bowles, Jeffrey V.
Corporate Authors: United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Ames Research Center
Other Authors: Waters, Mark H., Galloway, Thomas L.
Format: Book
Language:English
Published: Washington: NASA, 1976
Series:NASA technical note 8144
Subjects:
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100 1 |a Bowles, Jeffrey V. 
245 1 0 |a Thrust and wing loading requirements for short haul aircraft constrained by engine noise and field lenght/  |c Jeffrey V. Bowles, Mark H. Waters and Thomas L. Galloway 
260 |a Washington:  |b NASA,  |c 1976 
300 |a vi, 36 σ. :  |b εικ. ;  |c 28 εκ. 
490 0 |a NASA technical note  |v 8144 
504 |a Βιβλιογραφία: σ. 17 
650 0 |a Airplanes  |x Turbofan engines  |x Noise 
650 0 |a Airplanes  |x Turbojet engines  |x Mufflers 
650 0 |a Airplanes  |x Performance 
650 0 |a Flaps (Airplanes) 
650 0 |a Short take-off and landing aircraft 
700 1 |a Waters, Mark H. 
700 1 |a Galloway, Thomas L. 
710 |a United States  |b National Aeronautics and Space Administration 
710 0 |a United States.  |b National Aeronautics and Space Administration 
710 2 |a Ames Research Center 
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