A STOL Airworthiness Investigation Using Simulations of Representative STOL Aircraft

A simulator study of STOL airworthiness criteria for approach and landing was conducted using a series of different aircraft models. These models were selected to isolate a single parameter or characteristic for evaluation. Specific areas included in the study were: an evaluation of speed margins, a...

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Hauptverfasser: Rumold,Robert, Lehman,John M, Stapleford,Robert L, Hynes,Charles S, Scott,Barry C
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creator Rumold,Robert
Lehman,John M
Stapleford,Robert L
Hynes,Charles S
Scott,Barry C
description A simulator study of STOL airworthiness criteria for approach and landing was conducted using a series of different aircraft models. These models were selected to isolate a single parameter or characteristic for evaluation. Specific areas included in the study were: an evaluation of speed margins, a flight path margin evaluation, a study of flare and landing technique, the effects of touchdown zone constraints, an evaluation of two different turbulence models, an investigation of flight path/airspeed cross coupling, and a study of the effects of short-term flight path response. This report contains a detailed description of the simulation and the data obtained. These data include performance measures, pilot commentary, and pilot ratings.
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source DTIC Technical Reports
subjects Aircraft landings
Aircraft touchdown constraints
Airworthiness
Approach
Criteria
DOT/4 DZ/DA
DOT/5 D
Flight paths
Model tests
Performance tests
Pilots
Short takeoff aircraft
Simulation
Simulators
Turbulence
V/STOL
Velocity
title A STOL Airworthiness Investigation Using Simulations of Representative STOL Aircraft
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