A tabulation of section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for four swept wings having the same planform but different surface shapes. Emma Jean Landrum

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086 0 ⊔ ‡aNAS 1.14:D-1244
088 ⊔ ⊔ ‡aNASA-TN-D-1244
100 1 ⊔ ‡aLandrum, Emma Jean.
245 1 2 ‡aA tabulation of section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for four swept wings having the same planform but different surface shapes. ‡bEmma Jean Landrum.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Office of Technical Services, Dept. of Commerce], ‡c[1962]
300 ⊔ ⊔ ‡a36 p.: ‡bill. ; ‡c26 cm.
490 0 ⊔ ‡aNASA technical note ; ‡vNASA TN D-1244
500 ⊔ ⊔ ‡aCover title.
500 ⊔ ⊔ ‡a"April 1962."
500 ⊔ ⊔ ‡aAerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft; Stability and control; Stresses and loads.
504 ⊔ ⊔ ‡aIncludes bibliographical references.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 7 ‡aStresses and loads. ‡2nasat
650 ⊔ 7 ‡aStability and control. ‡2nasat
650 ⊔ 7 ‡aAircraft. ‡2nasat
650 ⊔ 7 ‡aAerodynamics, missiles and space vehicles. ‡2nasat
650 ⊔ 7 ‡aAerodynamics, aircraft. ‡2nasat
650 ⊔ 0 ‡aAirplanes ‡xWings, Swept-back ‡xDesign and construction.
650 ⊔ 0 ‡aCamber (Aerofoils)
650 ⊔ 0 ‡aAirplanes ‡xWings, Swept-back ‡xMathematical models.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ⊔ ⊔ ‡a011446794
DAT 0 ⊔ ‡a20101108131052.0 ‡b20141009010000.0
DAT 1 ⊔ ‡a20141112165512.0 ‡b2023-03-14T18:18:42Z
CAT ⊔ ⊔ ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
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