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 .- Washington, D. C.: National Aeronautics and Space Administration,  1959 
.- ( National Aeronautics and Space Administration NASA Technical Note   
<br/>NASA TR R-11: An approximation analytical method for studying entry into planetary atmospheres by Dean R. Chapman 44p NASA 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 NASA TR R-13: Effect of a stringer concentration due to a crack in a thin sheet by J. Lyell Sanders 10p NASA TR R-14: A method for calculation of hydrodynamic lift for submerged and planing rectangular lifting surfaces by Kenneth L. Wadlin 13p NASA TR R=15: Approximate analytical solutionsfor hypersonic flow overslender power law bodies by Harold Mirels 24p NASA TR R-16: Effects of mach number and wall temperature at mach numbers from 3 to 5 by Thorval Tendeland 15p NASA 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 NASA 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 NASA TR R-19: Theoretical analysisof thr longitudinal behavior of an automaticcaly controlled supersonic intercepeter during the attach phase by Ordway B. Gates 21p NASA TR R-20: Tire to surface friction coefficient measurements with A C-123B airplaneon various runwaysurfaces by Richard H. Sawyer 32p 
<br><U>Copy Details:</u><br> Acc. No.: <b>65619</b>, Full Call No.: ,   Item type:  Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN R 11-20<br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>