Ground effect (aerodynamics) (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "Ground effect (aerodynamics)" in English language version.

refsWebsite

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4nasa.gov

75^th place

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2web.archive.org

1^st place

1faa.gov

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607^th place

1soaneemrana.org

low place

1core.ac.uk

1,734^th place

1,312^th place

1archive.org

6^th place

1abbottaerospace.com

low place

1semanticscholar.org

11^th place

8^th place

1princeton.edu

741^st place

577^th place

1aviationweek.com

1,181^st place

736^th place

1aviation-safety.net

417^th place

408^th place

1flightsafetyaustralia.com

low place

1ntsb.gov

1,153^rd place

667^th place

abbottaerospace.com

"Aerodynamics of ROTOR CRAFT". ABBOTTAEROSPACE.COM. April 12, 2016. pp. 2–6.

archive.org

HANDBOOKS, OPERATIONAL READINESS, MISSION PROFILES, PERFORMANCE (ENGINEERING), PROPULSION SYSTEMS, AERODYNAMICS, STRUCTURAL ENGINEERING, Defense Technical Information Center (1974)

aviation-safety.net

Ranter, Harro. "ASN Aircraft accident de Havilland DH-106 Comet 1A CF-CUN Karachi-Mauripur RAF Station". aviation-safety.net.

aviationweek.com

"The NTSB’s John O’Callaghan, a national resource specialist in aircraft performance, noted that all aircraft stall at approximately 2-4 deg. lower AOA [angle of attack] with the wheels on the ground." (from NTSB Accident Report concerning loss of a swept wing business-class jet airplane in April 2011) Thin Margins in Wintry Takeoffs AWST, 24 December 2018

core.ac.uk

Saeed, B.; Gratton, G.B. (2010). "An evaluation of the historical issues associated with achieving non-helicopter V/STOL capability and the search for the flying car" (PDF) (February): 94. {{cite journal}}: Cite journal requires |journal= (help)

faa.gov

"Chapter 7 - Helicopter Performance" (PDF). Helicopter Flying Handbook. Federal Aviation Administration. 2020.

flightsafetyaustralia.com

Staff writers (October 25, 2019). "Reprise: Night of the Comet | Flight Safety Australia".

nasa.gov

ntrs.nasa.gov

Hall, Gordon R. (1971). MODEL TESTS OF CONCEPTS TO REDUCE HOT GAS INGESTION IN VTOL LIFT ENGINES(NASA CR-1863) (PDF) (Report). Nasa. p. 4.
Krishnamoorthy, V. (1971). AN ANALYSIS OF CORRELATING PARAMETERS RELATING TO HOT-GAS INGESTION CHARACTERISTICS OF JET VTOL AIRCRAFT (PDF) (Report). NASA. p. 8.
Mitchell, Kerry (1987). Proceedings of the 1985 NASA Ames Research Center's Ground-Effects Workshop (NASA Conference Publication 2462). Nasa. p. 4.^{[dead link]}

rotorcraft.arc.nasa.gov

Rotor raft Flying Handbook (PDF). Federal Aviation Administration. 2000. pp. 3–4. Archived from the original (PDF) on 2016-12-27. Retrieved 2021-11-03.

ntsb.gov

"Crash During Experimental Test Flight Gulfstream Aerospace Corporation GVI (G650), N652GD Roswell, New Mexico April 2, 2011" (PDF). www.ntsb.gov.

princeton.edu

catalog.princeton.edu

Williams, R.S. (1985). Addendum to AGARD report no. 710, Special Course on V/STOL Aerodynamics, an assessment of European jet lift aircraft. AGARD report; no. 710, addendum. p. 4. ISBN 9789283514893. {{cite book}}: |website= ignored (help)

semanticscholar.org

api.semanticscholar.org

Ameel, Frederick Donald (1979). "Application of Powered High Lift Systems to STOL Aircraft Design". p. 14. S2CID 107781224. {{cite web}}: Missing or empty |url= (help)

soaneemrana.org

Raymer, Daniel P. (1992). Aircraft Design: A Conceptual Approach (PDF) (2 ed.). American Institute of Aeronautics and Astronautics, Inc. ISBN 0-930403-51-7. Archived from the original (PDF) on 2019-07-04. Retrieved 2019-12-26. Section 20.6

web.archive.org

Raymer, Daniel P. (1992). Aircraft Design: A Conceptual Approach (PDF) (2 ed.). American Institute of Aeronautics and Astronautics, Inc. ISBN 0-930403-51-7. Archived from the original (PDF) on 2019-07-04. Retrieved 2019-12-26. Section 20.6
Rotor raft Flying Handbook (PDF). Federal Aviation Administration. 2000. pp. 3–4. Archived from the original (PDF) on 2016-12-27. Retrieved 2021-11-03.