Normalization of F/A-18E/F flight demonstrated dynamic minimum control airspeeds to reference conditions-Reference-Cited by-同舟云学术

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Normalization of F/A-18E/F flight demonstrated dynamic minimum control airspeeds to reference conditions

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Marks Bret¹,Melton, III Henry²,Lawrence Tom²

Affiliation:

1. Boeing Co., St. Louis, MO

2. U.S. Naval Air Systems Command, Patuxent River, MD

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-409

Reference19 articles.

1. Simulation , LPQ 1,000 HR Engines, Pilot Inputs Adjusted To HoldWings Level/ Duplicate Flight Test AOA

2. AC 165166 FLIGHT 405 RUN 45 TASK 3 MODSDF,JUN99AERO, PFQ New Engines, Pilot InputsAdjusted To HoldWings Level/ Duplicate FlightTest AOA MODSDF,JUN99AERO, LPQ 1,000 HR Engines, Pilot Inputs Adjusted To HoldWings Level/ Duplicate FlightTest AOA

3. „ -20-1 -40 - co ?60-Q.oU

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1. Investigation and Prediction of Steam-Induced Stall-Margin Reduction in Two Transonic Rotor Fans;Journal of Fluids Engineering;2014-09-04

2. Effect of Propeller Torque on Minimum-Control Airspeed;Journal of Aircraft;2006-09

3. A Review of Minimum Control Airspeed Test Methodologies for Carrier-Based Aircraft;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2005-06-19

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