000			02035nam a22002897a 4500
003			OSt
005			20220914121950.0
008			220914b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
110			_aWashington: National Aeronautics and Space Administration
245			_a-
260			_aWashington, D. C. _bNational Aeronautics and Space Administration _c1959
440			_aNational Aeronautics and Space Administration
440			_aNASA Technical Note
500			_aNASA TR R-11: An approximation analytical method for studying entry into planetary atmospheres by Dean R. Chapman 44p
500			_aNASA TR R-12: Effect of the proximity of the wing first bending frequency and the short period frequency on the airplane dynamic response factor by Carl R. Huss 20p
500			_aNASA TR R-13: Effect of a stringer concentration due to a crack in a thin sheet by J. Lyell Sanders 10p
500			_aNASA TR R-14: A method for calculation of hydrodynamic lift for submerged and planing rectangular lifting surfaces by Kenneth L. Wadlin 13p
500			_aNASA TR R=15: Approximate analytical solutionsfor hypersonic flow overslender power law bodies by Harold Mirels 24p
500			_aNASA TR R-16: Effects of mach number and wall temperature at mach numbers from 3 to 5 by Thorval Tendeland 15p
500			_aNASA TR R-17: Analysis of turbulent flow and heat transferon a flat plate at high mach numberswith variales fluid properties by R. G. Deissler 33p
500			_aNASA TR R-18: Several methods for aerodynamics reduction of static pressure sensing errors for aircraft at subsonic near sonic andlowsupersoni sppeds by Virgil S.Ritchie 23p
500			_aNASA TR R-19: Theoretical analysisof thr longitudinal behavior of an automaticcaly controlled supersonic intercepeter during the attach phase by Ordway B. Gates 21p
500			_aNASA TR R-20: Tire to surface friction coefficient measurements with A C-123B airplaneon various runwaysurfaces by Richard H. Sawyer 32p
942			_cTR
999			_c566118 _d566118