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1.
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EXPERIMENTAL STUDY OF THE PRESSURE AND HEAT-TRANSFER DISTRIBUTION ON A 70(DEGREE) SWEEP SLAB DELTA WING IN HYPERSONIC FLOW
by Bertram,Mitchel H | Everhart,Philip E. Material type:  Book Description: 122.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TR R-153 -] (1).
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2.
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Some simple solutions to the problem of predicting boundary layer self induced pressures [NASA TN D-798]
by Bertram, Mitchel H | Blackstock,Thomas A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 50p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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3.
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A SIMPLE METHOD FOR DETERMINING HEAT TRANSFER, SKIN FRICTION, AND BOUNDARY-LAYER THICKNESS FOR HYPERSONIC LAMINAR BOUNDARY-LAYER FLOWS IN A PRESSURE GRADIENT
by Bertram,Mitchel H | Feller,William V. Material type: Book Publisher: Nasa, Washington, D.C. 1959Availability: No items available Damaged (1).
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4.
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ENGINEERING PREDICATION OF TURBULENT SKIN FRICTION AND HEAT TRANSFER IN HIGH-SPEED FLOW.
by Cray,Aubery M | Bertram,Mitchel H. Material type: Book Description: 86.Publisher: Nasa, Washington, D.C. 1974Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7507] (1).
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5.
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HYPERSONIC LAMINAR VISCOUS INTERACTION EFFECTS ON THE AERODYNAMICS OF TWO-DIMENSIONAL WEDGE AND TRIANGULAR PLANFORM WINGS
by Bertram,Mitchel H. Material type: Book Description: 84.Publisher: Nasa, Washington, D.C. 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-3523] (1).
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6.
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CORRELATION GRAPHS FOR SUPERSONIC FLOW AROUND RIGHT CIRCULAR CONES AT ZERO YAW IN AIR AS A PERFECT GAS
by Bertram,Mitchel H. Material type: Book Description: 21.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2339] (1).
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7.
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CALCULATIONS OF COMPRESSIBLE AVERAGE TURBULENT SKIN FRICTION
by Bertram,Mitchel H. Material type: Book Description: 53.Publisher: Nasa, Washington, D.C. 1962Availability: No items available Damaged (1).
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8.
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Effects of boundary layer displacement and leading edge bluntness on pressure distribution, skin friction, and heat transfer of bodies at hypersonic speeds [NACA TN-4301]
by Bertram, Mitchel H | Henderson, Arthur. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 25p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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