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1.
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INFLUANCE OF LARGE POSITIVE DIHEDRAL ON HEAT TRANSFER TO LEADING EDGES OF HIGHLY SWEPT WINGS AT VERY HIGH MACH NUMBERS
by Cooper,Morton | Stainback,P Calvin. Material type:  Book Description: 18.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA MEMO 3-7-59L] (1).
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2.
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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. Material type: Book Description: 24.Publisher: Nasa, Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1246] (1).
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3.
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EXPERIMENTAL STUDIES OF HYPERSONIC BOUNDARY-LAYER TRANSITION AND EFFECTS OF WIND-TUNNEL DISTURBANCES
by Stainback,P Calvin,Wagner,Richard D | Owen,F Kevin. Material type: Book Description: 46.Publisher: Nasa, Washington, D.C. 1974Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7453] (1).
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4.
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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]
by Washington. National Aeronautics and Space Administration (NASA) | Stainback, P. Calvin. Material type: Book Description: 50p.Publisher: Washington NASA 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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5.
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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. Material type: Book Description: 30.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-184] (1).
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6.
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AERODYNAMIC HEATING IN THE VICINITY OF CORNERS AT HYPERSONIC SPEEDS
by Stainback,P Calvin | Weinstein,Leonard M. Material type: Book Description: 25.Publisher: Nasa, Washington, D.C. 1967Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4130] (1).
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7.
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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. Material type: Book Description: ,76.Publisher: NASA, WASHINGTON, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4961] (1).
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8.
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NASA Technical Note [NASA TN D-385]: A visual technique for determining qualitative aerodynamic heating rates on complex configurations
by Washington. National Aeronautics and Space Administration (NASA) | Stainback, P. Calvin. Material type: Book Description: 25p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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