Conceptual Design Studies of a V/STOL Civil Lift Fan Transport Including Effect of Size and Fan Pressure Ratio

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National Aeronautics and Space Administration, 1974 - Lift fans - 62 pages

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Contents

SELECTED AIRCRAFT CHARACTERISTICS
12
2
25
5
34

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Common terms and phrases

100 passenger 1968 AIA METHOD 200 NM VTOL aircraft configuration aircraft designed aircraft selected AIRFRAME COST angle approximately attitude control capability compliance control requirement cruise Mach number cruise speed CTOL current study DC-9 Type Empennage DESIGN CRUISE DIRECT OPERATING COST dispatch reliability DOLLARS ENGINE AIRCRAFT TASK engine configuration ETAC evaluation factors FAN PRESSURE RATIO fan thrust flight envelope ft² fuel fuselage gas generator inlet gross weight ground noise guideline changes height control HR/YR km/hr KTAS lb kg lead compensation MILE SEAT km mission requirements NASA nautical miles NM VTOL MISSION nozzle parameter payload performance pitch powered lift RELATIVE SEAT MILE Remote Lift Fan reverse thrust SEAT MILE SEAT SELECTED 4 ENGINE SELECTED AIRCRAFT shown in Figure stage length statute mile STOGW STOL takeoff and landing takeoff profile Task 1A thrust modulation thrust vectoring TOGW updated V/STOL aircraft V/STOL Lift Fan VTOGW wing yaw control

Bibliographic information

TitleConceptual Design Studies of a V/STOL Civil Lift Fan Transport Including Effect of Size and Fan Pressure Ratio
NASA contractor report
ContributorsMcDonnell Aircraft Company, Ames Research Center
PublisherNational Aeronautics and Space Administration, 1974
Original fromUniversity of Illinois at Urbana-Champaign
DigitizedApr 27, 2011
Length62 pages
  
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