PKK Library Search for 'au:"Burbank,Paige B"'

DISTRIBUTION OF HEAT TRANSFER ON A 10(DEGREE) CONE AT ANGLES OF ATTACK FROM 0(DEGREE) TO 15(DEGREE) FOR MACH NOS.OF 2.49 TO4.65 & A SOLUTION TO THE HEATTRANSFER EQU. THAT PERMITS COMPLETE MACHINE CAL.

By Burbank,Paige B, Hodge,B Leon. Nasa, Washington, D.C. 1959 . 45 , Bound With Nasa Memo 6-1-59l-6-29-59l

Place Hold on DISTRIBUTION OF HEAT TRANSFER ON A 10(DEGREE) CONE AT ANGLES OF ATTACK FROM 0(DEGREE) TO 15(DEGREE) FOR MACH NOS.OF 2.49 TO4.65 & A SOLUTION TO THE HEATTRANSFER EQU. THAT PERMITS COMPLETE MACHINE CAL.

HEAT-TRANSFER AND PRESSURE MEASUREMENTS OF A 1/7-SCALE MODEL OF A MERCURY CAPSULE AT ANGLES OF ATTACK FROM 0 DEGREE TO +- 20 DEGREE AT MACH NUMBERS OF 3.50 AND 4.44

By Taylor,Nancy L,Hodge,Ward F. Nasa, Washington, D.C. 1961 . 77 , Bound With Nasa Tm X-507-19,530-81 515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80

Place Hold on HEAT-TRANSFER AND PRESSURE MEASUREMENTS OF A 1/7-SCALE MODEL OF A MERCURY CAPSULE AT ANGLES OF ATTACK FROM 0 DEGREE TO +- 20 DEGREE AT MACH NUMBERS OF 3.50 AND 4.44

A METHOD FOR CALCULATING THE CONTOUR OF BODIES OF REVOLUTION WITH A PRESCRIBED PRESSURE GRADIENT AT SUPERSONIC SPEED WITH EXPERIMENTAL VERIFICATION

By Burbank,Paige B. Naca, Washington 1955 . 64 , Bound With Naca Tn 3550-3554,3556-3559

Place Hold on A METHOD FOR CALCULATING THE CONTOUR OF BODIES OF REVOLUTION WITH A PRESCRIBED PRESSURE GRADIENT AT SUPERSONIC SPEED WITH EXPERIMENTAL VERIFICATION

HEAT-TRANSFER AND DRESSURE MEASUREMENTS ON A FLAT-FACE CYLINDER AT A MACH NUMBER RANGE OF 2.49 TO 4.44

By Burbank,Paige B. Nasa, Washington, D.C. 1959 . 24 , Bound With Nasa Tm X-5-17, Lack No. 6-7,10-15,18

Place Hold on HEAT-TRANSFER AND DRESSURE MEASUREMENTS ON A FLAT-FACE CYLINDER AT A MACH NUMBER RANGE OF 2.49 TO 4.44

Heat-Transfer and Pressure Measurements on a flat-plate surface and heat-transfer measurements on attached protuberances in a supersonic turbulent boundary layer at mach numbers of 2.65, 3.51, and 4.44

By Burbank, Paige B. Washington NASA 1962 . 423p. , Bound with TN D-1371-1375

Place Hold on Heat-Transfer and Pressure Measurements on a flat-plate surface and heat-transfer measurements on attached protuberances in a supersonic turbulent boundary layer at mach numbers of 2.65, 3.51, and 4.44

NASA Technical Note [D-2741-2750]

Washington NASA 1965 , NASA T N D-2741 : Preliminary investigation of filament-wound glass-reinforced plastics and liners for cryogenic pressure vessels/ by Morgan P. Hanson, Hadley T. Richards, and Robert O. Hickel | NASA T N D-2742 : Experimental investigation of support interference on a blunt body of revolution at a mach number of approximately 20/ by Charles G. Miller | NASA T N D-2743 : Studies of fatigue crack growth in alloys suitable for elevated-temperature applications/ by C. Michael Hudson | NASA T N D-2744 : Atmospheric slant path transmission in the 15μ CO2 band/ S. Roland Drayson Special Note: This report prepared under contract No. NASr-54(03) by University of Michigan, Ann Arbor, Mich. | NASA T N D-2745 : Torsional vibration characteristics of a 1/5-scale model of saturn SA-1/ by John J. Catherine | NASA T N D-2746 : Model solar proton environments for manned spacecraft design/ by Jerry L. Modisette, Terence M. Vinson, and Alva C. Hardy | NASA T N D-2747 : Meteoroid environment for near-earth, cislunar, and near-lunar operations/ by Paige B. Burbank, Burton G. Cour-Palais, and William E. McAllum | NASA T N D-2748 : Special form of a generalized inverse of an arbitrary complex matrix/ by Henry P. Decell | NASA T N D-2749 : Dynamics of rotating cylindrical space station/ by Walter Krause Polstorff | NASA T N D-2750 : Radiation geometry factor between the earth and a satellite/ by Tommy C. Bannister

Place Hold on NASA Technical Note [D-2741-2750]