More by Clarence L. Gills
Theoretical Analysis of Total-pressure Loss and Airflow Distribution for Tubular Turbojet Combustors with Constant Annulus and Liner Cross-sectional Areas: Issues 1371-1380
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Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Lateral Control of Swept and Unswept Wings: Issues 1131-1140
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Wartime Report: L 1-787
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Report
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Technical Memorandum - National Advisory Committee for Aeronautics: Issues 1271-1280
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Wartime Report: L 1-787
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Wartime Report: L 1-787
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Report
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Annual Report of the National Advisory Committee for Aeronautics
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Annual Report of the National Advisory Committee for Aeronautics: Administrative Report Without Technical Reports
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Technical Note - National Advisory Committee for Aeronautics: Volumes 2475-2485
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Technical Note: Issues 1006-1013
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Technical Note - National Advisory Committee for Aeronautics: Issues 777-790
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Report
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Technical Note - National Advisory Committee for Aeronautics: Issues 2001-2010
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Research Abstracts: Issue 12
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Report
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Wartime Report: L 1-787
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