PKK Library catalog › Results of search for 'au:"Mack, Robert J."'

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- Carlson,Harry W, Barger,Raymond L (1)
- Dollyhigh, Samuel M (1)
- Mack, Robert J (2)
- Mack, Robert J. (1)
- Mack,Robert J (3)
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- Shrout, Barrett L, (1)
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- Aerodynamics (1)
- Parasol-Wing -- Body Combination (1)
- Sonic Boom -- Bodies of Revolution (1)

	1.	NASA Technical Note: WIND-TUNNEL INVESTIGATION OF SONIC-BOOM PRESSURE DISTRIBUTIONS OF BODIES OF REVOLUTION AT MACH 2.96, 3.83, AND 4.63 by Shrout, Barrett L \| Dollyhigh, Samuel M \| Mack, Robert J. Material type: Book Description: 32p.Publisher: Washington, D.C. NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1). Add to cart (remove)
	2.	NASA Technical Note: AERODYNAMIC CHARACTERISTICS OF A PARASOL-WING-BODY COMBINATION UTILIZING FAVORABLE LIFT INTERFERENCE AT MACH NUMBERS FROM 3.00 TO 4.63 by Morris, Odell A \| Mack, Robert J. Material type: Book Description: 36p.Publisher: Washington, D.C. NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1). Add to cart (remove)
	3.	APPLICATION OF SONIC-BOOM MINIMIZATION CONCEPTS IN SUPERSONIC TRANSPORT DESIGN by Carlson,Harry W, Barger,Raymond L \| Mack,Robert J. Material type: Book Description: 57.Publisher: Nasa, Washington, D.C. 1973Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7218 -] (1). Add to cart (remove)
	4.	NASA TN [D-5057] : NUMERICAL METHOD FOR EVALUATION AND UTILIZATION OF SUPERSONIC NACELLE-WING INTERFERENCE by Mack, Robert J. Description: 26p.Publisher: Nasa, Washington, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1). Add to cart (remove)
	5.	A STUDY OF METHODS WHICH PREDICT SUPERSONIC FLOW FIELDS FROM BODY GEOMETRY, DISTANCE, AND MACH NUMBER by Mack,Robert J. Material type: Book Description: 24.Publisher: Nasa,Washington, D.C. 1973Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7387] (1). Add to cart (remove)
	6.	EFFECTS OF LEADING-EDGE SWEEP ANGLE AND DESIGN LIFT COEFFICIENT ON PERFORMANCE OF A MDIFIED ARROW WING AT A DESIGN MACH NUMBER OF 2.6 by Mack,Robert J. Material type: Book Description: 49.Publisher: Nasa, Washington, D.C. 1974Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7753] (1). Add to cart (remove)

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