PKK Library Search for 'au:"STAINBACK,P CALVIN"'

INFLUANCE OF LARGE POSITIVE DIHEDRAL ON HEAT TRANSFER TO LEADING EDGES OF HIGHLY SWEPT WINGS AT VERY HIGH MACH NUMBERS

By Cooper,Morton. Nasa, Washington, D.C. 1959 . 18 , Bound With Nasa Memo 3-2-59l-3-6-59l,And 3-8-59l-3-17-59l Lack No. 9, 11, 13-14

Place Hold on INFLUANCE OF LARGE POSITIVE DIHEDRAL ON HEAT TRANSFER TO LEADING EDGES OF HIGHLY SWEPT WINGS AT VERY HIGH MACH NUMBERS

PRESSURE MEASUREMENT ON TWO 60 DEGREE SWEPT DELTA WINGS WITH BLUNT LEADING EDGES AND DIHEDRAL ANGLES OF 0 DEGREE AND 45 DEGREE AT A MACH NUMBER OF 4.95

By Stainback,P Calvin. Nasa, Washington, D.C. 1962 . 24 , Bound With Nasa Tn D-1241-45, 1247-50

Place Hold on PRESSURE MEASUREMENT ON TWO 60 DEGREE SWEPT DELTA WINGS WITH BLUNT LEADING EDGES AND DIHEDRAL ANGLES OF 0 DEGREE AND 45 DEGREE AT A MACH NUMBER OF 4.95

EXPERIMENTAL STUDIES OF HYPERSONIC BOUNDARY-LAYER TRANSITION AND EFFECTS OF WIND-TUNNEL DISTURBANCES

By Stainback,P Calvin,Wagner,Richard D. Nasa, Washington, D.C. 1974 . 46 , Bound With Nasa Tn D-7449-52,7454-58

Place Hold on EXPERIMENTAL STUDIES OF HYPERSONIC BOUNDARY-LAYER TRANSITION AND EFFECTS OF WIND-TUNNEL DISTURBANCES

NASA Technical Note [NASA TN D-549]: Heat-transfer measurements at a mach number of 4.95 on two 60 [degree] swept delta wings with blunt leading edges and dihedral angles of 0 [degree] and 45 [degree]

Washington NASA 1961 . 50p , Bound together NASA TN D-541 to 550 | Bound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862

Place Hold on NASA Technical Note [NASA TN D-549]: Heat-transfer measurements at a mach number of 4.95 on two 60 [degree] swept delta wings with blunt leading edges and dihedral angles of 0 [degree] and 45 [degree]

AN EXPERIMENTAL INVESTIGATION AT A MACH NUMBER OF 4.95 OF FLOW IN THE VICINITY OF A 90 DEGREE INTERIOR CORNER ALINED WITH THE FREE-STREAM VELOCITY.

By Stainback,P Calvin. Nasa, Washington, D.C. 1960 . 30 , Bound With Nasa Tn D-181-183,185-190.

Place Hold on AN EXPERIMENTAL INVESTIGATION AT A MACH NUMBER OF 4.95 OF FLOW IN THE VICINITY OF A 90 DEGREE INTERIOR CORNER ALINED WITH THE FREE-STREAM VELOCITY.

AERODYNAMIC HEATING IN THE VICINITY OF CORNERS AT HYPERSONIC SPEEDS

By Stainback,P Calvin. Nasa, Washington, D.C. 1967 . 25 , Bound With Nasa Tn D-4121-4129

Place Hold on AERODYNAMIC HEATING IN THE VICINITY OF CORNERS AT HYPERSONIC SPEEDS

EFFECT OF UNIT REYNOLDS NUMBER, NOSE BLUNTESS, ANGLE OF ATTACK, AND ROUGHNESS ON TRANSITION ON A 5 (DEGRE) HALF-ANGLE CONE AT MACH 8

By STAINBACK,P CALVIN. NASA, WASHINGTON, D.C. 1969 . ,76,,,,,, , Bound with NASA TN D-4962-4970

Place Hold on EFFECT OF UNIT REYNOLDS NUMBER, NOSE BLUNTESS, ANGLE OF ATTACK, AND ROUGHNESS ON TRANSITION ON A 5 (DEGRE) HALF-ANGLE CONE AT MACH 8

NASA Technical Note [NASA TN D-385]: A visual technique for determining qualitative aerodynamic heating rates on complex configurations

Washington NASA 1960 . 25p , Bound together NASA TN D-381 to 390 | Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611

Place Hold on NASA Technical Note [NASA TN D-385]: A visual technique for determining qualitative aerodynamic heating rates on complex configurations