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1.
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WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF A NONLIFTING VEHICLE SUITABLE FOR REENTRY
by Pearson,Albin O. Material type:  Book Description: 14.Publisher: Nasa, Washington, D.C. 1959Availability: No items available Damaged (1).
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2.
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AERODYNAMIC AND HYDRODYNAMIC CHARACTERISTICS OF A PROPOSED SUPERSONIC MULTIJET WATER-BASED HULL-TYPE AIRPLANE WITH A VARIABLE-INCIDENCE WING
by Petynia,William W, Pearson,Albin O | Fournier,Roger H. Material type: Book Description: 90.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-249 -] (1).
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3.
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STATIC LONGITUDINAL CHARACTERISTICS OF SEVERAL PROJECT MERCURY LAUNCH VEHICLES AT MACH NUMBERS BETWEEN 0.4 AND 6.8
by Church,Jemes D,Pearson,Albin O | Bernot,Peter T. Material type: Book Description: 48.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-433] (1).
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4.
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WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.50 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF A MODEL OF A PROJECT MERCURY CAPSULE
by Pearson,Albin O. Material type: Book Description: 28.Publisher: Nasa,Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-292] (1).
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5.
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WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.30 TO OF THE STATIC AERODYNAMIC CHARACTERISTICS OF MODIFIED MERCURY ESCAPE AND EXIT CAPSULE CONFIGURATIONS
by Pearson,Albin O. Material type: Book Description: 35.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-547] (1).
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6.
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HYDRODYNAMIC AND AERODYNAMIC CHARACTERISTICS OF A MODEL OF A SUPERSONIC MULTIJET WATER-BASED AIRCRAFT EQUIPPED WITH SUPERCAVITATING HYDROFOILS
by Mckann,Robert E,Blanchard,Lysse J | Pearson,Albin O. Material type: Book Description: 46.Publisher: Nasa, Washington, D.C. 1960Availability: No items available Damaged (1).
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7.
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WIND-TUNNEL CALIBRATIONS OF A COMBINED PITOT-STATIC TUBE, VANE-TYPE FLOW -DIRECTION TRANSMITTER, AND STAGNATION-TEMPERATURE ELEMENT AT MACH NUMBERS FROM 0.60 TO 2.87
by Richardson,Norman R | Pearson,Albin O. Material type: Book Description: 26.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-122] (1).
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8.
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WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER
by Pearson,Albin O. Material type: Book Description: 63.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-317] (1).
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9.
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Surface pressure distributions on 0.0628-scale models of proposed project fire space vehicles at Mach numbers from 0.25 to 4.63 [NASA TN D-1961]
by Pearson, Albin O. Material type: Book Description: 164p.Publisher: Washington, D.C. National Aeronautics and Space Administration [NASA] 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1961] (1).
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