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- 73499065 contributor B2357179.
- 73499065 created "19".
- 73499065 date "19".
- 73499065 date "1900".
- 73499065 dateCopyrighted "19".
- 73499065 description "--pt. 2. Experimental results for mach numbers 2.00 and 2.58.".
- 73499065 description "Includes bibliographical references.".
- 73499065 extent "v.".
- 73499065 isPartOf "Australia. Department of Supply. Aeronautical Research Consultative Committee. Report ACA -70".
- 73499065 isPartOf "Dept. of Supply. Australian Aeronautical Research Committee. Report ACA-70".
- 73499065 issued "19".
- 73499065 issued "1900".
- 73499065 language "eng".
- 73499065 publisher "[Melbourne] Dept. of Supply, Australian Aeronautical Research Committee,".
- 73499065 subject "629.13/008 s".
- 73499065 subject "Aerodynamics, Supersonic.".
- 73499065 subject "Airplanes Wings, Triangular.".
- 73499065 subject "Pressure.".
- 73499065 subject "TL507 .A8 no. 70, etc.".
- 73499065 tableOfContents "--pt. 2. Experimental results for mach numbers 2.00 and 2.58.".
- 73499065 title "Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow, by E. R. A. Landers.".
- 73499065 type "text".