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|a 0830-H-13 (online)
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|a NAS 1.14:D-6994
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| 099 |
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|a Online Government Document
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| 100 |
1 |
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|a Snyder, Melvin H.,
|c Jr,
|d 1921-
|e author.
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| 245 |
1 |
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|a Application of the leading-edge-suction analogy to prediction of longitudinal load distribution and pitching moments for sharp-edged delta wings /
|c by Melvin H. Snyder, Jr., and John E. Lamar.
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| 264 |
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1 |
|a Washington, D.C. :
|b National Aeronautics and Space Administration,
|c October 1972.
|
| 300 |
|
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|a 1 online resource (20 pages) :
|b illustrations.
|
| 336 |
|
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|a text
|b txt
|2 rdacontent
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| 337 |
|
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|a computer
|b c
|2 rdamedia
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| 338 |
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|a online resource
|b cr
|2 rdacarrier
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| 490 |
1 |
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|a NASA/TN ;
|v D-6994
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| 500 |
|
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|a "October 1972."
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| 504 |
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|a Includes bibliographical references (pages 10-11).
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| 513 |
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|a Technical note.
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| 536 |
|
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|a NASA Langley Research Center
|h 501-06-04-01
|
| 588 |
|
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|a Description based on online resource, PDF version; title from title page (NASA, viewed on June 23, 2021).
|
| 650 |
|
7 |
|a Aerodynamic loads.
|2 nasat
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| 650 |
|
7 |
|a Delta wings.
|2 nasat
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| 650 |
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|a Pitching (Aerodynamics)
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| 650 |
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0 |
|a Airplanes
|x Wings, Triangular.
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| 650 |
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|a Vortex-motion.
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| 650 |
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|a Aerodynamic load.
|2 fast
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| 650 |
|
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|a Airplanes
|x Wings, Triangular.
|2 fast
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| 650 |
|
7 |
|a Pitching (Aerodynamics)
|2 fast
|0 (OCoLC)fst01064896
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| 650 |
|
7 |
|a Vortex-motion.
|2 fast
|0 (OCoLC)fst01169197
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| 700 |
1 |
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|a Lamar, John E.,
|e author.
|
| 710 |
1 |
|
|a United States.
|b National Aeronautics and Space Administration,
|e issuing body.
|
| 710 |
2 |
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|a Langley Research Center.
|
| 830 |
|
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|a NASA technical note ;
|v D-6994.
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| 856 |
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|a Middle Tennessee State University
|b Main
|c James E. Walker Library
|d Electronic Resources
|t 0
|e NAS 1.14:D-6994
|h Superintendent of Documents classification
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