Lee-side flow over delta wings at supersonic speeds /

Saved in:

Bibliographic Details
Author / Creator:	Miller, David S., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, June 1985.
Description:	1 online resource (iii, 150 pages) : illustrations.
Language:	English
Series:	NASA/TP ; 2430 NASA technical paper ; 2430.
Subject:	Aerodynamics, Supersonic. Airplanes -- Wings, Triangular. Vortex-motion. Leading edges (Aerodynamics) Aerodynamics, Supersonic. Airplanes -- Wings, Triangular. Leading edges (Aerodynamics) Vortex-motion.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11618639

Hidden Bibliographic Details
Other authors / contributors:	Wood, Richard M., author. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body. Langley Research Center.
Notes:	"June 1985." Prepared at Langley Research Center. Includes bibliographical references (page 150). Technical paper. Langley Research Center 505-43-23-02 L-15888 Description based on online resource, PDF version; title from title page (NASA, viewed June 15, 2018).
Other form:	Print version: Miller, David S Lee-side flow over delta wings at supersonic speeds Microfiche: Miller, David S Lee-side flow over delta wings at supersonic speeds
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:2430

Similar Items