Conceptual Design Studies of Candidate V/STOL Lift Fan Commercial Short Haul Transport for 1980 - 1985 V/STOL Lift Fan Study

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1973 - 100 pages

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Contents

SUMMARY AND INTRODUCTION
11
11
65
41
85

Common terms and phrases

95 PNdB AIR MANEUVER AIRFRAME PRICE altitude BODY LENGTH bypass ratio climb control power cruise engines cruise fan cruise requirements cruise thrust CTOL direct operating costs DOC's drag coefficient eight-engine engine costs engine maintenance fan design fan failure FAN PRESSURE RATIO flaps flight path FUEL FLOW gross weight Hamilton Standard installed thrust integral fan integral lift fan LB/HR lift engines LIFT FAN M"-M low speed match maximum MODEL NOZZLE AREA RATIO OVERALL HEIGHT OVERALL LENGTH passenger payload percent pitch prop fan propulsion system rad/sec2 range remote fans remote lift fan REMOTE LIFT SYSTEM ROOT CHORD SEA LEVEL SEAT STATUTE MILE shown on Figure SPAN FT SPECIFIC FUEL CONSUMPTION STANDARD DAY takeoff and landing thrust required Thrust vectoring thrust weight ratio THRUST/WEIGHT TURBINE ENTRY TEMPERATURE V/STOL aircraft V/STOL Lift Fan V/STOL transport Vcon vertical takeoff VTO WEIGHT VTOGW VTOL mission VTOL STOL wing-loading

Bibliographic information

TitleConceptual Design Studies of Candidate V/STOL Lift Fan Commercial Short Haul Transport for 1980 - 1985 V/STOL Lift Fan Study
ContributorW. M. Eldridge
Published1973
Original fromNational Aeronautics and Space Administration (NASA)
DigitizedMay 20, 2010
Length100 pages
  
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