Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range /

Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range /

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Bibliographic Details
Author / Creator:Chapman, Dean R., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1952.
Description:1 online resource (44 pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 2787
Technical note (United States. National Advisory Committee for Aeronautics) ; 2787.
Subject:
Aerodynamic load.
Aerodynamics, Supersonic.
Aerofoils.
Drag (Aerodynamics)
Aerodynamic load.
Aerodynamics, Supersonic.
Aerofoils.
Drag (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12381225
Hidden Bibliographic Details
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"September 17, 1952."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 24).
Description based on online resource, PDF version; title from title page (TRAIL, viewed July 31, 2020).
Other form:Print version: Chapman, Dean R., Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/2787

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