Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted v-tail /

Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted v-tail /

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Bibliographic Details
Author / Creator:Margason, Richard J., author.
Imprint:Washington, D.C. : National Aeronautics and Space Administration, November 1968.
Description:1 online resource (179 pages) : illustrations.
Language:English
Series:NASA technical note ; NASA TN D-4856
NASA technical note ; D-4856.
Subject:
Short take-off and landing aircraft.
Boundary layer control.
Propellers, Aerial.
Airplanes -- Tail surfaces.
Aerodynamics.
Aerodynamics.
Airplanes -- Tail surfaces.
Boundary layer control.
Propellers, Aerial.
Short take-off and landing aircraft.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12674933
Hidden Bibliographic Details
Other authors / contributors:Gentry, Garl L., author.
United States. National Aeronautics and Space Administration, issuing body.
Langley Research Center.
Notes:"November1968."
Includes bibliographical references (page 16).
Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 6, 2020).
Other form:Print version: Margason, Richard J Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail
GPO item no.:0830-H-13 (online)
Govt.docs classification:NAS 1.14:D-4856

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